# 国际标准

EASA PTS-VPT-DSN、FAA EB105A/AC150-5390-2D、CASA AC139.V-01、ICAO Annex 14 Vol II/Doc 9261。

# ICAO 直升机场标准

# EASA Vertiport设计规范

# FAA Vertiport与直升机场标准

# FAA EB-105A Vertiport Design (2024)

## Memorandum

Date: December 27, 2024

To: All Airports Regional Division Managers

From: Michael A.P. Meyers, P.E. Manager, Airport Engineering Division, AAS-100

![a220f97a968ac987f0cd753f4871d1443e6f06345fab0a6cbb8a60a56c86aebe.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a220f97a968ac987f0cd753f4871d1443e6f06345fab0a6cbb8a60a56c86aebe.jpg)

Prepared by: Robert Bassey, P.E., AAS-110

Subject: Engineering Brief No. 105A, Vertiport Design, Supplemental Guidance to Advisory Circular 150/5390-2D, Heliport Design

This Engineering Brief (EB) provides standards and guidance for the planning, design, and construction of heliports serving vertical takeoff and landing (VTOL) aircraft that meet the reference aircraft criteria in Table 1-1. These facilities may also be called vertiports or vertiport heliports. Note that this EB will be subject to update as data, analysis, and VTOL aircraft and operations develop in the future.

This is a revision to the original EB 105 issued on September 21, 2022. Principal changes include adjustments to the infrastructure classification, landing area geometry, markings, the addition of a section on parking, and the creation of a downwash and outwash protection area:

1. Infrastructure Classification: Transitioned this EB to be supplement guidance to advisory circular (AC) 150/5390-2D, Heliport Design. Vertiports are a type of heliport with distinct specific requirements similar to hospital or prior permission required (PPR) heliports. The heliport design AC was established for heliports serving helicopters with single, tandem (front and rear) or dual (side by side) rotors. EB 105A provides guidance for vertiports (a type of heliport) serving aircraft with three or more propulsors.

2. Marking: Updated the vertiport marking to align with other classes of heliport infrastructure. Vertiports are distinguished with the addition of a “VTL” marking on the touchdown and liftoff area (TLOF). See paragraph 4.0.

3. Geometry: Laid the foundation for updating the landing area geometry, creating a subset of the controlling dimension (D) related to just the propulsion devices. Where D is the diameter of the smallest circle enclosing of the entire VTOL aircraft projections, RD is the smallest circle enclosing just the propulsion units, which for some vertical takeoff and landing (VTOL) designs may be smaller than D. The geometry of the TLOF and final approach and takeoff area (FATO) are now related to the RD rather than D. The safety area has decreased in size. See paragraph 2.0.

4. Parking: Created a new section on VTOL parking with larger parking positions that support air or hover taxiing to them rather than just ground taxiing. See paragraph 3.0.

5. Downwash and Outwash Caution Area: Added a downwash/outwash caution area (DCA). Refer to the Federal Aviation Administration (FAA) Technical Center research report DOT/FAA/TC-24/42, eVTOL Downwash and Outwash Surveys, on velocity findings for example distances for aircraft 7,000 lbs (3,175 kg) and less. See paragraph 2.5.

## Attachment

# ENGINEERING BRIEF #105A

# Vertiport Design, Supplemental Guidance to Advisory Circular 150/5390-2D, Heliport Design

## I Purpose.

This Engineering Brief (EB) specifies design guidance for public and private vertiports1 , including modification of existing helicopter and airplane landing facilities, and the establishment of new sites. Vertiports are a type of heliport.

For the purposes of this EB, “General Aviation” refers to all VTOL operations other than scheduled service (with the exception of unscheduled service with VTOLs with maximum takeoff weight (MTOW) greater than 12,500 pounds (lbs)). Vertiports fall under General Aviation but are distinct from General Aviation heliports and treated separately in this EB due to their specific requirements. General Aviation vertiports may be publicly or privately owned. Advisory circular (AC) 150/5390-2, Heliport Design, was established for heliports serving helicopters with single, tandem (front and rear) or dual (side by side) rotors. EB 105A provides guidance for vertiports (a type of heliport) serving aircraft with three or more propulsive units. Specifically, for the purposes of this document, the term VTOL refers to aircraft that are being certified as powered-lift or special class rotorcraft that meet the reference aircraft criteria and characteristics in Table 1-1.

At this time, the Federal Aviation Administration (FAA) is still collecting validated VTOL aircraft operational data and is transitioning from a prescriptive approach to a performance-based design approach with the recommendations in this EB. This EB is a living document that serves as the FAA’s standards and guidance. An AC will be developed to adapt and address new aircraft and technology as performance data is received. This EB will be cancelled concurrent with the publication of the AC.

Figures in this document are general representations and are not to scale.

## II Background.

The FAA has identified a need for guidance for vertiports to be utilized by VTOL aircraft.

The FAA’s previous AC on Vertiport Design, published on May 31, 1991, provided guidance for vertiport design and was based on civil tiltrotors modeled after military tiltrotor technology. However, the intended aircraft were never used commercially, and the AC was cancelled on July 28, 2010.

This EB provides the standards and guidance needed to support initial infrastructure development for VTOL operations. This guidance is correlated to the reference VTOL aircraft described in paragraph 1.5. The Reference Aircraft represents a VTOL aircraft that integrates certain design characteristics of emerging aircraft and all-engine operating performance characteristics of three currently in development and made available for testing. The Reference Aircraft has been coordinated with multiple FAA lines of business (LOBs). The Reference Aircraft is used to specify certain performance and design characteristics that informed the guidance in this EB.

There is currently limited demonstrated performance data on how VTOL aircraft operate. Research efforts are underway to better understand the performance capabilities and design characteristics of emerging VTOL aircraft. The FAA will develop a performancebased AC on vertiport design in the future, as additional performance data is gleaned about these emerging VTOL aircraft. The FAA Office of Airports is working with the FAA Aircraft Certification Service to develop a mechanism for VTOL aircraft manufacturers to demonstrate equivalent helicopter landing accuracy during their certification process.

Future guidance is expected to address more advanced operations including autonomy, facilities operating in instrument meteorological conditions (IMC), different propulsion methods, density, frequency, and complexity of landing facilities. To support the development of a comprehensive AC, additional research is required to garner VTOL aircraft performance data on downwash/outwash, failure conditions or degradation of performance, landing precision (in all azimuth wind capabilities), and nominal climb/descend/approach gradients. The data will be collected and used by the FAA research team to fill in aircraft information gaps. This will require continued coordination within the FAA across the various LOBs, as well as external collaboration with manufacturers and other stakeholders. A proponent interested in sharing data must work with the FAA Office of Airports Safety and Standards division to participate in validated empirical data collection that addresses these performance data gaps.

## III Application.

This EB is intended as standards and guidance for vertiport design until a more comprehensive performance-based AC is developed. The guidance herein is not legally binding in its own right and will not be relied upon by the FAA as a separate basis for affirmative enforcement action or other administrative penalty. Conformity with this guidance, as distinct from existing statutes, regulations, and grant assurances, is voluntary only, and nonconformity will not affect existing rights and obligations. The standards and guidance contained in this EB are practices the FAA recommends establishing for an acceptable level of safety, performance, and operation in the design of new civil vertiports, and for modifications of existing helicopter and airplane landing facilities. This EB does not prescribe any guidance for the operation of a VTOL aircraft.

The vertiport design criteria in this EB is intended for special class rotorcraft and powered-lift aircraft with three or more propulsive units and a pilot on board, that fly in visual meteorological conditions (VMC), and that meet the characteristics in Table 1-1. These design recommendations are for a single aircraft using the touchdown and lift off (TLOF) area, final approach and takeoff area (FATO) area, and Safety Area at one time. The ingress and egress path should be kept clear. At all Federally-obligated facilities, the proponent is required to confirm the ingress and egress path is clear. See paragraph 2.6.

For heliport facilities that serve single, tandem (front and rear), or dual (side by side) rotor helicopters and intend to accommodate emerging VTOL aircraft, the proponent should follow the recommendations in this EB and mark the facility as a vertiport. Vertiports may accommodate helicopters that fit within the size and maximum takeoff weight (MTOW) of the design VTOL. This guidance applies to new vertiports and heliports that are modified to accept VTOL aircraft.

Proponents of vertiport facilities who intend to serve VTOL aircraft that do not meet the performance criteria and design characteristics of the Reference Aircraft included in this EB should begin coordination with the applicable FAA Regional or Airports District Office early in the planning and design process. These facilities will be subject to review on a case-by-case basis.

## IV Questions.

Contact the FAA Office of Airports – Airports Safety and Standards Airport Engineering Division, AAS-100 Robert.Bassey@faa.gov for any questions about this EB.

## V Effective Date.

This EB becomes effective as of the date the associated memorandum is signed by the Manager, FAA Airport Engineering Division, AAS-100.

## Table of Contents

1.0 Introduction. ........ ................................................................................. 9   
1.1. EB Guideline Justification. . .............................................. ..... 9   
1.2. Explanation of Terms. ........ ........................................................... 9   
1.3. Airspace Approval Process and Coordination. ..................................................... 12   
1.4. State/Local Role. .. ............................... ..... 13   
1.5. Reference Aircraft. .. .... 14   
2.0 Vertiport Design and Geometry. ................................. ................ ..... 16   
2.1. Overview. .... ............................................................................ ..... 16   
2.2. TLOF Guidance. .... ................................................................... .... 17   
2.3. FATO Guidance. ...... .......................................................................................... 21   
2.4. Safety Area Guidance. ...... ............................................... ....... 23   
2.5. Downwash/Outwash (DWOW) Caution Guidance. ...................................... ..... 24   
2.6. VFR Approach/Departure Guidance.. ......... .... 26   
3.0 Vertiport Taxiways and Parking. .... ............................................ ...... 31   
3.1. Vertiport Parking. . .............................................. ..... 31   
4.0 Marking, Lighting, and Visual Aids. ... ................................................ .... 33   
4.1. General. . ................................................................. ...... 33   
4.2. Identification Symbol... .............................................. ....... 35   
4.3. TLOF Size/Weight Limitation Box. ... ........................... ...... 35   
4.4. Flight Path Alignment Optional Marking and Lighting. .............................. ..... 39   
4.5. Lighting. ...... ................... ....... 41   
4.6. Identification Beacon. . ........................................ ..... 47   
4.7. Wind Cone. . ... 47   
5.0 Charging and Electric Infrastructure. ................................................................... ....... 48   
5.1. Standards. .... ....................................................... ....... 48   
5.2. Other Information. ..... ................................................................................ ...... 51   
6.0 On-Airport Vertiports. ...... ........................... ....... 52   
6.1. On-Airport Location of TLOF. ......... ...................................................... ........ 52   
6.2. On-Airport Location of FATO.. ............................................ ..... 52   
7.0 Site Safety Elements. . ............................................. .... 55   
7.1. Fire Fighting Considerations.. ... 55   
7.2. Security and Safety. . .... 55   
7.3. Wind and Turbulence.. .. 56   
7.4. Weather Information.. ... 57   
7.5. Winter Operations. ... .... 57   
7.6. Access to Vertiports by Individuals with Disabilities.. .. 57   
7.7. Electromagnetic Effects. .. .... 58   
Appendix A. Air Traffic Considerations for Siting Vertiports On or Near Existing   
Airports ..... ... 60   
A.1. Definitions...... ..... 60   
A.2. Assumptions.... ..... 61   
A.3. Air Traffic Considerations. . ... 61   
A.4. Vertiport Siting Scenarios... .... 62   
Appendix B. Acronyms and Terms ...... .... 65

## Figures

Figure 1-1: Controlling Dimension. . 10   
Figure 2-1: Relationship and Dimensions of TLOF, FATO, and Safety Area.... . 17   
Figure 2-2. VTOL Landing Gear Loading: Gradients and Pavement . .. 20   
Figure 2-3: Vertiport Gradients and Rapid Runoff Shoulder .. ... 21   
Figure 2-4: DCA Caution Sign ... ... 26   
Figure 2-5: VFR Vertiport Approach/Departure Surfaces.. . 28   
Figure 2-6: VFR Vertiport Curved Approach/Departure and Transitional Surfaces.. .. 29   
Figure 4-1: Standard Vertiport Identification Marking . ... 34   
Figure 4-2: Heliport Identification Symbol .. .. 36   
Figure 4-3: Form and Proportions of 36-inch (914 mm) Numbers for Marking Size and Weight   
Limitations . ... 37   
Figure 4-4: Form and Proportions of 18-inch (457 mm) Numbers for Marking Size and Weight   
Limitations .. ... 38   
Figure 4-5: Flight Path Alignment Marking and Lighting.. ... 40   
Figure 4-6: TLOF/FATO Lighting .. .. 43   
Figure 4-7: Elevated Vertiport Configuration Example . . 44   
Figure 6-1: Example of an On-airport Vertiport. . 54   
Figure 6-2: Vertiport Caution Sign. . 56   
Figure 6-3. Vertiport EMI Hazard Marking . .. 58   
Figure A-1. Siting Vertiports on or Near Existing Airports . ... 63

## Tables

Table 1-1: Reference Aircraft .. 14   
Table 2-1: Takeoff and Landing Area Minimum Dimensions . 16   
Table 4-1: Perimeter Lighting Intensity and Distribution.. .. 42   
Table 6-1: Recommended Minimum Distance between Vertiport FATO Center to Runway   
Centerline for VFR Operations... . 53

## 1.0 Introduction.

## 1.1. EB Guideline Justification.

Limited data is available on VTOL aircraft operational characteristics, performance, maneuverability, downwash/outwash impacts, and vertiport data needs. Consequently, this EB is limited to pilot-on-board, visual flight rule (VFR) operations, and VTOL aircraft that have the characteristics and performance of the Reference Aircraft described in paragraph 1.5.

Heliports provide the most analogous present-day model for vertiports. However, there are design differences between traditional helicopters and VTOL aircraft that create specific, unique infrastructure requirements. VTOL aircraft have varied configurations including unique types and numbers of propulsion systems. As a result, the conversion ratio in AC 150/5390-2 of 0.83 × the controlling dimension (D) being used to calculate the main rotor diameter of the design helicopter is not representative of the diverse characteristics associated with the various VTOL aircraft being developed. In addition, there persists a lack of validated data on the performance capabilities of VTOL aircraft.

The anticipated Advanced Air Mobility (AAM) tempo of operations, complexity of operations, and overall number of aircraft in the National Airspace System (NAS) is expected to be high in some cases and would be influenced by local conditions in each of the operating markets. These operations are also anticipated to include commuter and ondemand (i.e., Part 135 and Part 91) operations and may require unique operational safety and infrastructure requirements similar to other types of heliports.

The FAA has begun an operational testing campaign on VTOL aircraft. Initial observations based on engagement with the aircraft that have been part of the FAA’s operational testing campaign have shown that these aircraft generally have the ability to hover out of ground effect and utilize highly augmented stability and control for operation and landing. Data gaps exist amongst the varied design configurations of these aircraft and the environmental conditions they may operate in. This ensuing EB represents a continued move toward performance-based design criteria leveraging the data collected in the FAA’s campaign. However, while valuable data has been collected, more data is needed for comprehensive performance-based design criteria.

This EB is intended for aircraft that have hover out of ground effect (HOGE) capability. If the vertiport Design VTOL aircraft is known not to perform HOGE, the sponsor should coordinate directly with the FAA to determine alternative vertiport sizing for that Design VTOL aircraft.

## 1.2. Explanation of Terms.

Terms used in this EB:

1. Approach/Departure Path: The approach/departure path is the flight track that VTOL aircraft follow when landing at or taking off from a vertiport. See paragraph 2.6.2.

2. Battery: One or more electrically connected cells, assembled in a single container having positive and negative terminals. A battery may include inter-cell connectors and other devices.

3. Battery pack: Two or more battery systems.

4. Battery system: Comprised of the battery, the battery charger, and any protective, monitoring, and alerting circuitry or hardware inside or outside of the battery. It also includes vents (where necessary) and packaging.

5. Controlling dimension (D): The diameter of the smallest circle enclosing the entire VTOL aircraft projection on a horizontal plane, including all possible configurations with rotors/propellers turning, if applicable. See Figure 1-1.

Figure 1-1: Controlling Dimension  
![933d4996866684340edd75404a5228a7d6f68e6491f48d9206653b3fa510b90d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/933d4996866684340edd75404a5228a7d6f68e6491f48d9206653b3fa510b90d.jpg)

6. Design VTOL aircraft: The Design VTOL aircraft is the largest VTOL aircraft with three or more propulsive units that is expected to operate at a vertiport. This Design VTOL aircraft is used to size the TLOF, FATO and Safety Area. Note that the Design VTOL aircraft is different from the Reference Aircraft used to define the performance and design criteria in this EB.

7. Downwash/Outwash (DWOW): The downward and outward movement of air caused by the action of rotating rotor blade, propeller, or ducted fan. When this air strikes the ground or some other surface, it causes a turbulent outflow of air from the aircraft.

8. Downwash/Outwash Caution Area (DCA): An operational area that is identified to protect persons and property from downwash and outwash (including jet blast or propwash) that may meet or exceed 34.5 mph (55.5 kph).

9. Elevated vertiport: A vertiport is considered elevated if it is located on a rooftop or other elevated structure where the TLOF and FATO are at least 30 inches (0.8 m) above the surrounding surface (a ground-level vertiport with the TLOF on a mound is not an elevated vertiport).

10. Effective transitional lift (ETL): The pronounced increase in translational lift during transition to forward flight due to the rotor/propeller experiencing a significantly decreased induced airflow.

11. Failure condition (FC): FC is one or more failures, which affects the aircraft’s ability to generate lift or thrust and results in a consequential state that has an impact for a given flight phase.

12. Final approach and takeoff area (FATO): The FATO is a defined area over which the aircraft completes the final phase of the approach to a hover or a landing, and from which the aircraft initiates takeoff.

13. Ground Effect: A condition of usually improved performance encountered when the aircraft is operating very close to the ground or a surface. It results from a reduction in upwash, downwash, and/or blade tip vortices, which provide a corresponding decrease in induced drag.

14. Hover: The word “hover” applies to an aircraft that is airborne and remaining in one place at a given altitude over a fixed geographical point regardless of wind.

15. Hover out of ground effect (HOGE): The ability to achieve hover without the benefit of the ground or a surface.

16. Imaginary surface(s): The imaginary planes defined in Title 14 Code of Federal Regulations (CFR) Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, centered about the FATO and the approach/departure paths, which are used to identify the objects where notice to and evaluation by the FAA is required.

17. Obstruction to air navigation: Any fixed or mobile object, including a parked aircraft, of greater height than any of the heights or imaginary surfaces presented in subpart C of 14 CFR Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace.

18. Powered-lift: Defined in 14 CFR Part 1 as a heavier-than-air aircraft capable of vertical takeoff, vertical landing, and low speed flight that depends principally on engine-driven lift devices or engine thrust for lift during these flight regimes and on nonrotating airfoil(s) for lift during horizontal flight.

19. Reference Aircraft: The Reference Aircraft represents a VTOL aircraft that integrates certain design characteristics of emerging aircraft currently in development and performance characteristics of three currently in development and made available for testing. The Reference Aircraft is used to specify certain performance and design characteristics that informed the vertiport design guidance in this EB.

20. Rotor Diameter (RD): The largest length of all the rotors from tip to tip. It can be computed by finding the diameter of the smallest circle enclosing all the lift producing propulsion units, including their propellers, rotors, fans, etc., on a horizontal plane, while the aircraft is in the vertical takeoff or landing configuration, with rotors/propellers/fans turning, if applicable. The RD must also incorporate all landing gear and surface touch points. See Figure 1-1.

21. Safety Area: The Safety Area is a defined area surrounding the FATO intended to reduce the risk of damage to aircraft accidentally diverging from the FATO.

22. Translational Lift: Translational lift is the improved rotor/propeller efficiency resulting from directional flight.

23. Touchdown and liftoff area (TLOF): The TLOF is a load-bearing, generally paved, area centered in the FATO on which the aircraft performs a touchdown or liftoff.

24. Vertiport: An area of land, water, or a structure used, or intended to be used, to support the landing, takeoff, taxiing, parking, and storage of powered-lift aircraft or other aircraft that vertiport design and performance standards established by the Administrator can accommodate.†

25. Vertiport elevation: The highest elevation of all usable TLOFs within the vertiport expressed in feet above mean sea level (MSL).

## 1.3. Airspace Approval Process and Coordination.

For vertiport development on federally obligated airports, the infrastructure or equipment must be depicted on the Airport Layout Plan (ALP). See AC 150/5070-6, Airport Master Plans. For vertiport development on airports or heliports identified under § 77.9(d), at least 45 days before the start date of the proposed construction or alteration or the date an application for a construction permit is filed (whichever is earliest), a sponsor must submit a Form 7460-1, Notice of Proposed Construction or Alteration, and obtain a nonobjectionable airspace determination. The FAA’s review of the ALP and airspace determination must be completed prior to the start of construction.

For development on non-federally obligated airports or heliports or for non-federally funded standalone vertiport sites, and in compliance with 14 CFR Part 157, Notice of Construction, Alteration, Activation, and Deactivation of Airports, the proponent must submit FAA Form 7480-1, Notice for Construction, Alteration and Deactivation of Airports, at least 90 days in advance of the day that construction work is to begin on the takeoff and landing facility (see § 157.5 for other scenarios). Note: Airspace determination is not tied to this 90-day advance notice. Given the nascence of the AAM industry, the FAA highly encourages that engagement with the appropriate FAA regional or district office begin before the submission of the Form 7480-1, but an FAA evaluation is predicated on the submitted Form 7480-1.

For non-federally funded heliport facilities that are being modified in geometry in accordance with the design criteria in this EB, the sponsor must submit a new Form

7480-1 at least 90 days in advance of the day that work is to begin. See 14 CFR Part 157. The Form 7480-1 can be submitted electronically as a Digital 7480 at https://adip.faa.gov. The FAA’s Flight Standards Service Office will determine when to do an onsite evaluation using risk-based analysis (see FAA Order 8900.1, Flight Standards Information Management System).

## 1.4. State/Local Role.

Many state departments of transportation, aeronautics commissions, or similar authorities require prior approval and, in some instances, a license or permit to establish and operate landing facilities. Those seeking to establish a vertiport should first contact their   
respective state or local transportation or aeronautics departments or commissions for specifics on applicable licensing or permitting. Several states also administer Federal assistance programs and may be staffed to provide technical advice. Municipalities often staff a help desk to provide assistance on navigating local permitting processes. Contact information for state aviation agencies is available at   
https://www.faa.gov/airports/resources/state\_aviation/. State agencies may also choose to educate local officials throughout their state and advocate for the harmonization of applicable local policies.

In addition to state requirements, many local communities have enacted zoning ordinances, building and fire codes, and various land entitlement processes that guide development approval and operation, such as conditional use permits. Some communities have developed codes or ordinances regulating environmental issues such as noise and air pollution. Therefore, communities, proponents, or sponsors seeking to establish a publicor private-use vertiport should make early contact with:

• local officials or agencies representing the local land use/zoning board;

• the fire, police, or sheriff's department; and

• stakeholders who represent the area where the vertiport is to be located.

For optimal success, the FAA encourages early and continued engagement across all project phases. This can help identify and mitigate potential conflicts, ensuring smoother project approvals.

State regulators, departments of transportation, and local communities can also use the guidance and best practices outlined in this EB when reviewing a proposed vertiport facility or developing independent standards.

In addition to state and local coordination, vertiport proponents are encouraged to coordinate potential sites with any nearby landing facilities and aviation stakeholders. Lack of early coordination can cause airspace, operational, safety, capacity, and financial impacts. While the FAA will review all new vertiport proposals for the safe and efficient utilization of navigable airspace by aircraft and the safety of persons and property on the ground, early coordination with these entities may offer early insights into airspace and capacity conflicts before investments are made.

## 1.5. Reference Aircraft.

The Reference Aircraft integrates the design characteristics of many emerging VTOL aircraft and the performance characteristics of three currently in development. The Reference Aircraft is used to specify certain performance and design characteristics that informed the vertiport design in this EB.

Emerging VTOL aircraft models are evolving rapidly with OEMs approaching aircraft certification from a wide range of different designs. While aircraft classifications are useful in takeoff and landing area design and airspace analysis, new VTOL aircraft concepts vary significantly in terms of design, aircraft dimensions, performance, and operational characteristics. Furthermore, these new VTOL aircraft do not have an established operating history and have not yet received FAA airworthiness certification. However, OEM engagement has revealed some common characteristics among VTOL aircraft prototypes including multiple propulsion systems, HOGE capability, and highly augmented stability and control.

The vertiport design guidance in this EB relies on design characteristics and performance capabilities of preproduction aircraft until there is adequate research on these emerging aircraft to develop a performance-based AC. Accordingly, the aircraft features and performance capabilities listed in Table 1-1 create a Reference Aircraft to inform this EB. The design characteristics, performance, and operating conditions that make up the reference VTOL aircraft will be reviewed in the future as the FAA continues to engage with emerging VTOL aircraft manufacturers.

Table 1-1: Reference Aircraft
<table><tr><td>Design Characteristics</td><td>Criteria</td></tr><tr><td>Propulsion</td><td>Electric battery driven, utilizing distributed electric propulsion</td></tr><tr><td>Propulsive units</td><td>3 or more</td></tr><tr><td>Battery systems</td><td>2 or more</td></tr><tr><td>MTOW</td><td>12,500 1bs (5,670 kg) or less</td></tr><tr><td>Controlling Dimension (CD)</td><td>50 feet (15.2 m) or less</td></tr><tr><td>Flight Control</td><td>Highly augmented stability and control</td></tr><tr><td>Operating Conditions</td><td></td></tr><tr><td></td><td>Criteria Land-based (ground or elevated) – no amphibian or float</td></tr><tr><td>Operation location</td><td>operations</td></tr><tr><td>Pilot</td><td>On board</td></tr><tr><td>Flight conditions</td><td>VMC</td></tr><tr><td>Performance</td><td>Criteria</td></tr><tr><td>Hover</td><td>Hover out of ground effect (HOGE) in normal operations</td></tr><tr><td>Takeoff</td><td>Vertical</td></tr><tr><td>Landing</td><td>Vertical from a steady state hover</td></tr></table>

## 2.0 Vertiport Design and Geometry.

## 2.1. Overview.

The takeoff and landing area design and geometry contained in this EB includes the TLOF, the FATO, and the Safety Area. The dimensions for these areas are presented in Table 2-1 and are based on the dimension D or RD of the Design VTOL aircraft as defined for each vertiport facility (see Figure 1-1). The FAA Office of Airports is working with the FAA Aircraft Certification Service to develop a mechanism and target for aircraft developers to, as an option, demonstrate landing accuracy. The ability to demonstrate equivalent helicopter landing accuracy to this target will support a reduced non-load-bearing FATO and, at a minimum, a 1 RD TLOF infrastructure requirement. ‡ The sizing requirements contained in Table 2-1 will continue to be applied at landing facilities catering to aircraft that do not or cannot demonstrate the target landing accuracy during type certification. A future performance-based TLOF size will incorporate the aircraft observed landing precision, while ensuring all propulsors can remain over a loadbearing surface. These sizing requirements may be modified as additional VTOL operational testing is performed. See Figure 2-1 for the relationship among the TLOF, FATO, and Safety Area.

Table 2-1: Takeoff and Landing Area Minimum Dimensions
<table><tr><td rowspan=1 colspan=1>Element</td><td rowspan=1 colspan=1>Dimension(length and width or diameter)</td></tr><tr><td rowspan=1 colspan=1>TLOF</td><td rowspan=1 colspan=1>1RD</td></tr><tr><td rowspan=1 colspan=1>FATO</td><td rowspan=1 colspan=1>2RD</td></tr><tr><td rowspan=1 colspan=1>Safety Area</td><td rowspan=1 colspan=1>2.5D</td></tr></table>

Figure 2-1: Relationship and Dimensions of TLOF, FATO, and Safety Area  
![2c73c8d3f60b20ce4a9fec334d0d76e214c11b7ed05a5ec8cfd9a9893344b5fd.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2c73c8d3f60b20ce4a9fec334d0d76e214c11b7ed05a5ec8cfd9a9893344b5fd.jpg)

## 2.2. TLOF Guidance.

The TLOF is a load-bearing, generally paved, area centered in the FATO on which the VTOL aircraft performs a touchdown or liftoff. The following guidelines apply to the TLOF:

1. Located at ground level, on elevated structures§ , or at rooftop level.

2. On level terrain or a level structure.

3. Clear of penetrations and obstructions to the transitional surfaces.

4. Load-bearing (static and dynamic for Design VTOL aircraft). See Figure 2-2.

a. Supports the static load of the Design VTOL aircraft and/or any ground support vehicles, whichever is more demanding for pavement design. The static loads are equal to the aircraft’s maximum takeoff weight applied through the total contact area of the landing gear.

b. Supports the dynamic loads based on 150 percent of the maximum takeoff weight of the Design VTOL aircraft. For design purposes, assume the dynamic load at 150 percent of the maximum takeoff weight applied over the whole landing gear for a landing gear with wheels, and at the single point of contact for a landing gear with skids.

c. Accounts for rotor/propeller downwash load in load-bearing capacity.

5. Centered within its own FATO and Safety Area.

6. Circular, square, or rectangular in shape\*\*. The TLOF should have the same shape as the FATO and Safety Area. A FATO and Safety Area can be rectangular with square TLOF.

7. Opposing sides of the FATO and Safety Area are equidistant to the center of the TLOF.

8. Minimum length and width (or diameter for circular) as outlined in Table 2-1.

9. Meets general surface characteristics and pavement guidelines including the following:

a. Has a paved or aggregate-turf surface (see AC 150/5370-10, Standard Specifications for Construction of Airports, Items P-217, Aggregate-Turf Runway/Taxiway, and P-501, Cement Concrete Pavement).

b. Use Portland cement concrete (PCC) when feasible for ground-level facilities. An asphalt surface is less desirable for VTOLs as it may rut under the wheels or skids of a stationary VTOL. This has been a factor in some rollover accidents. In addition, sections of asphalt have also been known to adhere to skids only to fall off after takeoff creating a hazard to vehicles, buildings, and persons on the ground.

c. Has a roughened pavement finish (e.g., brushed or broomed concrete) to provide a skid-resistant surface for VTOL aircraft and a non-slippery footing for people.

d. Elevations between any paved and unpaved portions of the TLOF and FATO are equal.

e. Surface is stabilized to prevent erosion or damage from rotor/propeller downwash or outwash from VTOL aircraft operations. (Find guidance on pavement design and soil stabilization in AC 150/5320-6, Airport Pavement Design and Evaluation, and AC 150/5370-10.)

f. Preferred surface of elevated TLOFs is concrete. Preferred material for elevated structures is metal or coated metal with an approved coating. If the surface is conductive, it may need to be insulated and/or grounded to the extent feasible to eliminate the threat of conducting electricity in cases of a short circuit or lightning strike. If the surface is metal, it should be grounded. Insulation is permissible if grounding is not feasible. Construct rooftop and other elevated TLOFs of metal, concrete, or other materials subject to local building codes.

g. Elevated TLOFs comply with 29 CFR § 1926.34, Means of Egress, and 29 CFR § 1910.25, Stairways, as applicable. See National Fire Protection Association (NFPA) 418, Standard for Heliport and Vertiports.

10. Gradient provides positive drainage (between -0.5 and -2.0 percent) off of and away from the pavement, as shown in Figure 2-3. If gradient cannot be met, and edge drains are used, then drainage systems should meet NFPA 415, Standard on Airport Terminal Buildings, Fueling Ramp Drainage, and Loading Walkways, requirements.

11. For rooftop or other elevated TLOFs, ensure that:

a. The FATO and TLOF are at or above the elevation of the adjacent Safety Area.

b. Elevator penthouses, cooling towers, exhaust vents, fresh-air vents, and other elevated features or structures do not affect VTOL aircraft operations or penetrate the TLOF, FATO, Safety Area, approach surface, or transition surface.

c. Fresh air vents for any attached building are not impacted by landing facility operations.

d. See paragraph 7.3, Wind and Turbulence.

Figure 2-2. VTOL Landing Gear Loading: Gradients and Pavement  
![6af01e146c32a77946b3f45176f66231e5fa818b4afc03c4f1870e5d40a75690.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6af01e146c32a77946b3f45176f66231e5fa818b4afc03c4f1870e5d40a75690.jpg)

Figure 2-3: Vertiport Gradients and Rapid Runoff Shoulder  
![25609580bd44861cdf205164db1f8c6f1cac490d1e8445c1da39258cf33fa8a8.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/25609580bd44861cdf205164db1f8c6f1cac490d1e8445c1da39258cf33fa8a8.jpg)  
The slope direction is based on the topography of the site.

Grade the TLOF, FATO, and Safety Area to provide positive drainage of the entire area for the TLOF, FATO, and Safety Area.

2:1 maximum Safety Area gradient for vertiports at ground level or where applicable at elevated structures.

## 2.3. FATO Guidance.

The FATO is a defined area over which the VTOL aircraft completes the final phase of the approach to a hover or a landing and from which the aircraft initiates takeoff. The following guidelines apply to the FATO:

1. Located at ground level, on elevated structures, or at rooftop level.

2. Clear with no penetrations or obstructions except for navigational aids that are fixedby-function (e.g., flight path alignment marking and lighting, approach lighting, TLOF lights)†† which should be of the lowest mass practicable and frangiblymounted objects no higher than 2 inches (51 mm) above the adjacent TLOF elevation, to the extent practicable. See AC 150/5220-23, Frangible Connections.

3. Load-bearing (static and dynamic for Design VTOL aircraft), including the following features:

a. Supports the static loads of the Design VTOL aircraft and/or any ground support vehicles, whichever is more demanding for pavement design. The static loads are equal to the aircraft’s maximum takeoff weight applied through the total contact area of the landing gear.

b. Supports the dynamic loads based on 150 percent of the maximum takeoff weight of the Design VTOL aircraft. For design purposes, assume the dynamic load at 150 percent of the maximum takeoff weight applied over the whole landing gear for a landing gear with wheels, and at the single point of contact for a landing gear with skids.

c. Downwash load is accounted for in load-bearing capacity.

4. Centered within its own Safety Area.

5. Minimum length and width (or diameter for circular) as outlined in Table 2-1.

6. The same geometric shape as the $\mathrm { T L O F ^ { \ddagger } }$ and Safety Area, except that the FATO and Safety Area can be rectangular with a square TLOF.

7. Design the distance between the opposing sides of the TLOF, FATO and Safety Area perimeters to be equidistant to the TLOF.

8. Meets general surface characteristics and pavement guidelines including the following:

a. Paved or aggregate-turf surface (see AC 150/5370-10, Items P-217, Aggregate-Turf Pavement and P-501, Cement Concrete Pavement).

b. Use Portland cement concrete (PCC) when feasible for ground-level facilities. An asphalt surface is less desirable for VTOLs as it may rut under the wheels or skids of a stationary VTOL. This has been a factor in some rollover accidents. In addition, sections of asphalt have also been known to adhere to skids only to fall off after takeoff creating a hazard to vehicles, buildings, and persons on the ground.

c. Has a roughened pavement finish (e.g., brushed or broomed concrete) to provide a skid-resistant surface for VTOL aircraft and a non-slippery footing for people.

d. Elevations between any paved and unpaved portions of the FATO are equal.

e. Surface is stabilized to prevent erosion of damage from rotor/propeller downwash or outwash from VTOL aircraft operations. (Find guidance on pavement design and soil stabilization in AC 150/5320-6 and AC 150/5370-10.)

f. Preferred surface of elevated FATO is concrete. If the surface is metal, it must be insulated/grounded to the extent feasible to eliminate the threat of conducting electricity in the case of a short circuit or lightning strike.

g. Elevated FATOs should be metal or concrete and comply with 29 CFR § 1926.34 and 29 CFR § 1910.25, as applicable.

9. The FATO surface prevents loose stones and any other flying debris caused by rotor/propeller downwash or outwash.

10. Gradient provides positive drainage (between 1.5 and 5.0 percent) off of and away from the pavement, with a minimum 10-foot wide (3 m wide) rapid runoff shoulder sloped between 3.0 and 5.0 percent, as shown in Figure 2-3. Design a negative gradient of not more than 2 percent in any areas where a VTOL is expected to land. If gradient cannot be met, and edge drains are used, then drainage systems should meet NFPA 415 requirements.

11. The edge of the FATO abutting the TLOF is the same elevation as the TLOF.

12. If the FATO is located on a rooftop or other elevated structures, ensure that:

a. The FATO and TLOF elevations are at or above the elevation of the adjacent Safety Areas.

b. The FATO is above the level of any obstacle in the Safety Area that cannot be removed.

c. Title 29 CFR § 1910.28, Duty to Have Fall Protection and Falling Object Protection, requires that the provision of fall protection if the platform is elevated 4 feet (1.2 m) or more above its surroundings. The FAA recommends such protection for all platforms elevated 30 inches (0.8 m) or more.

d. Does not use permanent railings or fences that would be safety hazards, such as those obstructing or penetrating an imaginary surface, during aircraft operations.

e. Safety nets that meet state and local regulations, are at least 5 feet (1.5 m) wide, and meet the following criteria can be used as one potential solution to protect against falls and falling objects:

i. The insides and outside edges of the nets are fastened to a solid structure.

ii. The net is constructed of materials that are resistant to environmental effects and is inspected annually for integrity.

iii. The net has a load carrying capability of 25 lbs per square foot (122 kg/sq m).

iv. The net is located at or below the edge elevation of the FATO.

v. The net is attached to the outer perimeter frame of the FATO.

## 2.4. Safety Area Guidance.

The Safety Area is a defined area surrounding the FATO intended to reduce the risk of damage to VTOL aircraft unintentionally diverging from the FATO. The following guidelines apply to the Safety Area:

1. Located at ground level, on elevated structures, at rooftop level, and can extend over water or in clear airspace.

2. Clear with no penetrations or obstructions except for navigational aids that are fixedby-function§§, which must be on frangible mounts. See AC 150/5220-23. Note: See paragraph 2.3.

3. For elevated TLOFs, no fixed objects within the Safety Area project above the FATO except those fixed-by-function which must be on frangible mounts. See AC 150/5220-23. Note: See paragraph 2.3.

4. Minimum length and width (or diameter for circular) as outlined in Table 2-1.

5. The same geometric shape as the TLOF and FATO, except a FATO and Safety Area can be rectangular with a square TLOF.

6. Design the distance between the opposing sides of the TLOF, FATO and Safety Area perimeters to be equidistant regardless of the shape of the TLOF.

7. If at ground level, the surface prevents loose stones and any other flying debris caused by downwash or outwash.

8. If at ground level, gradient provides positive drainage away from the FATO no steeper than 2:1, horizontal units and vertical units, respectively. See Figure 2-3.

9. On rooftop or other elevated FATOs, meets requirements contained in Title 29 CFR § 1910.28.

## 2.5. Downwash/Outwash (DWOW) Caution Guidance.

Downwash is the airflow created by the propulsion units producing lift in vertical flight. When the downwash hits the ground, it moves horizontally as outwash. The downwash and outwash created from the propulsion units of VTOL aircraft can be dangerous to people, property, equipment, and other aircraft. This downward and outward flow can result in ground surface erosion, wake recirculation, foreign object debris (FOD) and wind hazards.

Air velocities of approximately 34.5 mph (55.5 kph) or greater can impact vertiport safety\*\*\*. For vertiport planning purposes, DCAs should be established anywhere that wind velocity can potentially meet or exceed 34.5 mph (55.5 kph). These DCAs should be established in the form of operational boundaries, or areas of restriction/control on movement of persons during VTOL operations. The DCA should be in effect during any VTOL operations creating DWOW. The DCA may be a different size depending on the aircraft operating at the time. Vertiport operators should utilize the largest DCA size for the aircraft operating at the facility to determine distances used in the design considerations, signage, or movement restrictions. Vertiport development, landscaping, and other facility elements located inside the DCA should be designed and managed to mitigate objects that can become FOD or projectiles.

Through research, the FAA has identified the need for the DCA to extend beyond the safety area. Given research findings, the FAA William J. Hughes Technical Center is continuing to collect data and will update research report DOT/FAA/TC-24/42, eVTOL Downwash and Outwash Surveys, as wind velocities at various distances become available for aircraft 7,000 lbs (3,175 kg) or less.††† For heavier aircraft, the proponent will need to work directly with the FAA to determine appropriate sizing for the DCA.

The design of the DCA should consider that, in addition to the hover-over-the-landing point, DWOW will be prevalent whenever the VTOL is operating, including while taxiing and in parking areas. The combined risk from an aviation safety and occupational health and safety perspective may require supervision of vehicular and pedestrian traffic during VTOL movements, provision of robust maintenance and FOD prevention processes, and safeguarding of the DCA from future development to reduce the likelihood of injury or third-party damage. See Figure 2-4.

The as-built environment around the vertiport should be considered when establishing the DCA because certain types of structures may result in narrow venturi effect channels where the DWOW velocity is increased. Even moveable objects like parked vehicles can cause these venturi effect channels.

The primary way to mitigate the risks of DWOW to bystanders is to physically prohibit them from entering the DCA while it is in effect. The DCA can extend beyond the boundaries of the vertiport itself, and appropriate measures should be taken to mitigate the risks of DWOW in these areas. However, these measures must not become obstacles or promote the undesired venturi effect, which may increase risk to both bystanders and aircraft. Winds recirculating back to the aircraft can impact control inputs, particularly during critical phases of flight, and structures near the TLOF can create turbulence patterns that may not be reflected by wind cones. This can be either of a wall type – ideally with an upwards deflective curve on the inside to allow outwash to dissipate rather than recirculate back to the aircraft – or alternative methods such as slat structures / blast screens may be used, which are especially helpful for walkways in the vicinity of the vertiport.

# CAUTION

![8a307afad7a5d73e83559c6649c0840cf16cb4d4ac689b42ff0e22cc7fcf2541.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8a307afad7a5d73e83559c6649c0840cf16cb4d4ac689b42ff0e22cc7fcf2541.jpg)

# Strong Winds Strong winds may occur while aircraft are operating

## 2.6. VFR Approach/Departure Guidance.

2.6.1. VFR Approach/Departure and Transitional Surfaces.

The imaginary surfaces defined in 14 CFR Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, for heliports are applicable to vertiports and include the primary surface, approach, and transitional surfaces. Part 77 establishes standards and notification requirements for objects affecting navigable airspace. This notification provides the basis for:

evaluating the effect of construction or alteration on aeronautical operating procedures;

• determining the potential hazardous effect of proposed construction on air navigation;

• identifying mitigating measures to enhance safe air navigation; and

aeronautical charting for new objects.

The following applies to these imaginary surfaces:

1. The primary surface is synonymous with the FATO. This surface is a horizontal plane at the elevation of the established vertiport elevation.

2. The approach surface (and, by reciprocal, the departure surface) begins at the edge of the FATO (vertiport primary surface) with the same width as the primary surface and extends outward and upward for a horizontal distance of 4,000 feet (1,219 m) where its width is 500 feet (152 m). The slope of the approach surface is 8:1, horizontal units and vertical units, respectively.

3. The transitional surfaces extend outward and upward from the lateral boundaries of the primary surface and from the approach surfaces at a slope of 2:1, horizontal units and vertical units, respectively, for 250 feet (76 m) measured horizontally from the centerline of the primary and approach surfaces.

4. The approach, transitional, and primary surfaces should be clear of penetrations (with the exception of navigational aids that are fixed by function) unless an FAA aeronautical study determines penetrations to any of these surfaces not to be hazards. See Part 77.9(d) to determine when notification is required to initiate when aeronautical studies are conducted.

Figure 2-5 and Figure 2-6 show these surfaces for straight-in and curved approaches, respectively.

Figure 2-5: VFR Vertiport Approach/Departure Surfaces  
![973f9ee51dfe5409460421e1a8da505f624af0a5b7f6e94503197938665e862e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/973f9ee51dfe5409460421e1a8da505f624af0a5b7f6e94503197938665e862e.jpg)  
The preferred approach/departure surface is based on the predominant wind direction. Where a reciprocal approach/departure surface is not possible in the opposite direction, use a minimum 135-degree angle between the two surfaces.

Figure 2-6: VFR Vertiport Curved Approach/Departure and Transitional Surfaces  
![6b2a84b4dcc08b04e314cd3c0ef43094ffe592787ed14ad6b39eeff9c9e23d0d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6b2a84b4dcc08b04e314cd3c0ef43094ffe592787ed14ad6b39eeff9c9e23d0d.jpg)  
Use any combination of straight portions of one curved portion using the following formula: S + R ≥ 1,886 ft (575 m) and R ≥ 886 ft (270 m), where S is the length of the straight portion(s) and R is the radius of the turn. Note that any combination ≥ 1,886 ft (575 m) will work.  
The minimum total length of the centerline of the straight and curved portion is 4,000 ft (1,219 m).  
VTOL takeoff performance may be reduced in a curve. Consider a straight portion along the takeoff climb surface prior to the start of the curve to allow for acceleration.

## 2.6.2. VFR Approach/Departure Path.

The approach/departure path is the flight track that VTOL aircraft follow when landing at or taking off from a vertiport. The following guidelines apply to the approach/departure path(s):

1. Preferred approach/departure paths are aligned with the predominant wind direction as much as possible, to avoid downwind operations and keep crosswind operations to a minimum.

2. More than one approach/departure path is provided. They should be reciprocal in magnetic heading or at least 135 degrees apart.

3. Additional approach/departure paths are based on an assessment of the prevailing winds or separated from the preferred flight path by at least but not limited to 135 degrees.

4. All approach and departure paths are free of obstructions.

5. The approach/departure paths must assure 8:1 horizontal units and vertical units.

6. To the extent practicable, design vertiport approach/departure paths to be independent of approaches to, and departures from, active runways if separate vertiport takeoff and landing areas are needed.

7. The approach and departure path may be curved but only the VFR approach/departure and transitional surfaces outlined in paragraph 2.6.1 are addressed in 14 CFR Part 77, Safe, Efficient Use and Preservation of the Navigable Airspace. Therefore, while they may be used, curved approaches are not evaluated by the FAA for the effect of objects (temporary or permanent, existing or new) on aeronautical operating procedures. These curved approaches are also not considered in aeronautical charting for new objects.

See Figure 2-4 for a visual depiction of this guidance.

## 3.0 Vertiport Taxiways and Parking.

Further research is needed to understand VTOL taxiing and parking needs. In future guidance, taxiway guidance will be included. If necessary, in the interim, vertiports designed for ground taxiing can follow AC 150/5300-13 Taxiway Guidelines for Group 1 aircraft. For hover/air taxi, vertiport design should follow taxiway guidance in AC 150/5390-2 for the General Aviation type and include a DCA as described in paragraph 2.5. Consider VTOL turn radius when designing taxi intersections and parking for wheeled VTOLs. When designing parking positions, consider safety and fire mitigation measures for charging operations (see paragraph 5.0).

## 3.1. Vertiport Parking.

If more than one VTOL at a time is expected at a vertiport, design the facility with an area specifically designated for parking multiple VTOLs. The size of this area depends on the number and size of specific VTOLs to be accommodated. It is not necessary that every parking position accommodate the Design VTOL. Design the individual parking positions to accommodate the VTOL sizes and weights expected to use the parking position at the facility. Use the largest VTOL expected to use a parking position to determine the separation between parking positions intended for VTOL of different sizes.

Use the Design VTOL to determine the separation between parking positions and taxiways/taxilanes when using AC 150/5300-13. Use the Design VTOL to determine the separation between parking positions and taxi routes when using AC 150/5390-2. If the parking area is designed as one large apron, use the nearest parking position to determine separation distance.

1. Design the parking positions to support the static loads of the VTOL intended to use the parking area.

2. For parking positions that will allow hover and/or air taxi operations, the parking position should be no smaller than the FATO size and meet dynamic FATO loadbearing requirements. Ground vehicle loads should also be taken into consideration.

3. Design parking areas as one large, paved apron or as individual paved parking positions.

4. Consider the turn radius of VTOLs when designing taxi intersections and parking positions for wheeled VTOLs.

5. Locate aircraft parking areas outside of approach/departure surfaces. However, as an option, allow aircraft parking areas under the transitional surfaces.

6. Vertiport parking positions should be no smaller than the VTOL aircraft’s maximum width and maximum length plus a minimum of 0.28 × D, or at least 10 feet (3 m) clearance between aircraft and/or fixed objects. Alternatively, the parking position may be a polygon outlining the aircraft's geometry projected on the ground plus a minimum of 0.28 × D or at least 10 feet (3 m) clearance between aircraft and/or fixed objects. If turning the aircraft on the parking position is required, the size of the parking position should account for the additional space required for turning.

7. Additional factors may influence increasing the clearance values between aircraft and/or fixed objects such as an operator’s ground service equipment (GSE) work area envelope, charging stations/equipment, equipment storage, and the slope of the passenger boarding ramp in accordance with the Americans with Disabilities Act (ADA) (42 U.S.C. § 12101, et al.), when applicable.

8. Ensure GSE and vulnerable equipment is stowed away after use to prevent it from posing a tripping risk for people or FOD risk for aircraft.

9. Consider fire fighting response to lithium battery incidents. Due to the risk of thermal runaway propagation to nearby aircraft or structures, increased clearance and response measures may be necessary to mitigate these hazards.

## 3.1.1. Walkways.

1. Provide marked ingress/egress walkways.

2. Locate passenger walkways to minimize passenger exposure to various risks, including DWOW, during passenger loading and unloading.

## 3.1.2. Tiedowns.

1. Install recessed tiedowns to accommodate extended or overnight parking of based or transient VTOLs.

2. Ensure tie-downs will not pose a tripping hazard. As an option, highlight each tiedown point with a bright contrasting color of paint for pedestrian safety.

3. Ensure any depression associated with the tiedowns is of a diameter not greater than half the width of the smallest VTOL landing wheel anticipated to be operated on the vertiport surface.

4. Tie-down locations will vary depending on aircraft configurations.

## 4.0 Marking, Lighting, and Visual Aids.

This section provides guidance on marking, lighting, and visual aids that identify the facility as a vertiport. This guidance applies to new vertiports or to heliports that are modified to vertiports.

## 4.1. General.

The following general guidelines apply to markings:

1. Paint or preformed materials define the TLOF and FATO within the limits of those areas. See AC 150/5370-10, Item P-620, for specifications.

2. Reflective paint and retroreflective markers are optional and should be used with caution, as overuse of reflective material can be blinding to a pilot when using landing lights and/or night vision goggles. Federal Specification TT-B-1325, Federal Specification Beads (Glass Spheres) Retro-Reflective, provides technical specifications for reflectorizing markings. AC 150/5370-10 provides information on application rates.

3. Outlining markings and lines with a 2 to 6-inch (55-152 mm)-wide line of a contrasting color is an option to enhance conspicuity for day, night, and night vision operations.

4. TLOF perimeter marking is a 12-inch-wide (305 mm wide) solid white line.

5. TLOF size and weight limitation box is included on a TLOF with a hard surface (described in paragraph 4.3) and as an option on a TLOF with a turf surface.

6. FATO perimeter is marked by 12-inch-wide (305 mm wide) dashed white lines that are 5 feet (1.5 m) in length with end-to-end spacing of 5 to 6 feet (1.5 to 1.8 m) apart.

7. An optional touchdown/positioning circle (TDPC) marking provides guidance to allow a pilot to touch down in a specific position within the TLOF. This marking is intended for the pilot's seat to be over the marking, the undercarriage to be inside the load-bearing area (LBA), and all parts of the VTOL to be clear of any obstacle by a safe margin.

8. A TDPC marking is a yellow circle with an inner diameter of 1/2 RD and a line width of 18 inches (0.5 m). Locate a TDPC marking in the center of a TLOF. See Figure 4- 1.

See Figure 4-1 for a visual depiction of the standard vertiport marking.

Figure 4-1: Standard Vertiport Identification Marking  
![54642f6829eb9f530959f9e6ccd36c250e6aea4aad245ab8cc6fa25f62f5d2ea.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/54642f6829eb9f530959f9e6ccd36c250e6aea4aad245ab8cc6fa25f62f5d2ea.jpg)  
Figure is configured for 50-foot (15.2 m) TLOF.  
Solid and dashed white lines are 12 inches (305 mm) in width. Dashed lines are 5-foot (1.5 m) in length with 5-6-foot (1.5-1.8 m) spaces. Solid yellow TDPC circle is 18 inches (0.5 m) in width.  
See Figure 4-2 for details on the TLOF size/weight limitation box.  
See Figure 4-2 for details on the “H” and “VTL”.

## 4.2. Identification Symbol.

The heliport identification symbol and vertiport identification marking identify the location as a vertiport, marks the TLOF, and provides visual cues to the pilot. Vertiport facilities should use the “H” shown in Figure 4-2. Also see Figure 4-2 for dimensional standards for these markings. Guidelines for this marking include:

1. Locate the “H” in the center of the TLOF and orient it on the axis of the primary preferred approach/departure path.

2. Place a one-foot-wide bar 2 feet (0.6 m) below the “H”, the width of the “H”, when it is necessary to distinguish the preferred approach/departure direction. See Figure 4-1.

3. A "VTL" marking must be used to indicate a Vertiport. Text height is a minimum of   
3 feet (0.9 m) and a maximum of 5 feet (1.5 m). The preferred height is 5 feet (1.5 m).

## 4.3. TLOF Size/Weight Limitation Box.

The TLOF size/weight limitation box indicates the controlling dimension (maximum length or width) and the maximum takeoff weight of the Design VTOL aircraft that can use the vertiport. Weight limitation boxes should meet the following guidance:

1. The letters “RD” and the weight, in imperial units, of the Design VTOL aircraft that the vertiport is designed to accommodate are in a box in the lower right-hand corner of a rectangular TLOF, or on the right-hand side of the symbol of a circular TLOF, when viewed from the preferred approach direction.

2. The numbers are black on a white background.

3. The top number is the maximum takeoff weight of the Design VTOL aircraft in thousands of pounds for the Design VTOL the TLOF will accommodate. It is centered in the top half of the box.

4. The bottom number is the controlling dimension of the Design VTOL aircraft, is centered in the bottom half of the box, and is preceded by the letters “RD.”

5. A TLOF without a weight limit is marked with a diagonal line extending from the lower left-hand corner to the upper right-hand corner in the upper section of the TLOF size/weight limitation box.

See Figure 4-2 for details on the TLOF size/weight limitation box, and Figure 4-3 and Figure 4-4 for details on the form and proportions of the numbers and letters specified for these markings.

Figure 4-2: Heliport Identification Symbol  
![ec654b530ab955b7baccde268206c6911e3b8118e4d244dd6e685273adc81533.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ec654b530ab955b7baccde268206c6911e3b8118e4d244dd6e685273adc81533.jpg)

The minimum size of the box is 5 ft (1.5 m) square. Where possible, increase this dimension to a 10 ft (3 m) square for improved visibility.

For hospital marking alternatives, refer to AC 150/5390-2.

Figure 4-3: Form and Proportions of 36-inch (914 mm) Numbers for Marking Size and Weight Limitations  
![f2b9ba1094dad939e99012b5eb0962d7bca02d8fefb2ff13e4bcb12e53520086.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f2b9ba1094dad939e99012b5eb0962d7bca02d8fefb2ff13e4bcb12e53520086.jpg)

Figure 4-4: Form and Proportions of 18-inch (457 mm) Numbers for Marking Size and Weight Limitations  
![9da20688473825847bfbefe92bc8387d2943bb430377e91d4c8969824d87a55a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9da20688473825847bfbefe92bc8387d2943bb430377e91d4c8969824d87a55a.jpg)

## 4.4. Flight Path Alignment Optional Marking and Lighting.

Flight path alignment marking and lighting is optional and includes markings and/or lights when it is desirable and practicable to indicate available approach and/or departure flight path direction(s). Guidance for optional flight path alignment marking and lighting includes:

1. The shaft of each arrow is 1.5 ft (0.5 m) wide and at least 10 feet (3 m) long.

2. The arrow heads are 5 feet (1.5 m) wide and 5 feet (1.5 m) tall.

3. The color of the arrow must provide good contrast against the background color of the surface. Provide a contrasting border around the arrows if needed to increase visibility for the pilot.

4. An arrow pointing toward the center of the TLOF depicts an approach direction.

5. An arrow pointing away from the center of the TLOF depicts a departure direction.

6. In-pavement flight path alignment lighting is recommended. See paragraph 4.5 for additional guidance. For elevated lights, if the TLOF light conflicts with a flight path alignment light, remove the conflicting flight path alignment light fixture.

7. For a vertiport with a flight path limited to a single approach direction or a single departure path, the arrow marking is unidirectional (i.e., one arrowhead only). For a vertiport with only a bidirectional approach/takeoff flight path available, the arrow marking is bidirectional (i.e., two arrowheads).

8. Flight path alignment arrow lighting is recommended for night operations and includes a minimum of three lights spaced 5-10 feet (1.5 to 3 m) apart. These lights may extend across the TLOF, FATO, Safety Area, or any suitable surface in the immediate vicinity of the FATO or Safety Area, if necessary.

See Figure 4-5 for additional guidance.

Figure 4-5: Flight Path Alignment Marking and Lighting  
![c24367b69217c7328cbbea9fe00f71d16395be39394715dbfcf4cdd5e4451e72.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c24367b69217c7328cbbea9fe00f71d16395be39394715dbfcf4cdd5e4451e72.jpg)  
Figure is configured for 50-foot (15.2 m) TLOF.  
Arrowheads have constant dimensions.  
If necessary, adjust stroke length to match length available. Minimum length = 10 ft (3 m).  
Light type: omnidirectional green lights, Type L-861H or L-852H.  
If necessary, locate the lights outside of the arrow.  
In-pavement flight path alignment lighting is recommended.  
See paragraph 4.4 for guidance on flight path alignment markings.  
Flight path alignment marking and lighting may extend into the TLOF.

## 4.5. Lighting.

Lighting is required for vertiports that support night operations. The lighting should enable the pilot to both establish the location of the vertiport and identify the perimeter of the operational area. In-pavement lighting is preferred to elevated lighting. The following guidelines apply to lighting:

## 4.5.1. General.

For additional guidance on perimeter lighting for surface level vertiports, see Figure 4-6.   
For guidance for lighting for elevated vertiports, see Figure 4-7 and Figure 4-8.

1. Use FAA type L-861H elevated omnidirectional green and L-852H in-pavement omnidirectional green light fixtures for TLOF and FATO perimeter, flight path alignment, and approach/landing direction lighting applications. The specifications for these light fixtures will be found in AC 150/5345-46, Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures, and EB 67, Light Sources Other Than Incandescent and Xenon For Airport and Obstruction Lighting Fixtures. See AC 150/5390-2 for additional information.

2. The elevated light emitting diode (LED) vertiport fixture and LED in-pavement fixtures are identified as L-861H (L) and L-852H (L), respectively. Some LED light fixtures may not be compatible with the use of some night vision goggle systems.

3. Perimeter light fixtures must meet chromaticity requirements for “aviation green” per SAE AS 25050, Colors, Aeronautical Lights and Lighting Equipment, General Requirements, when using incandescent lights. For light fixtures that use LEDs, see the standards in EB 67.

4. Photometric standards for perimeter light fixtures are included in Table 4-1. See AC 150/5345-46 for detailed measurement methods and standards.

5. Elevated perimeter light fixtures will be installed in a load-bearing light base (L-868, Size B) or non-load-bearing light base (L-867, Size B) per AC 150/5345-42, Specification for Airport Light Bases, Transformer Housings, Junction Boxes, and Accessories. Shallow base type light bases will not be used.

6. Installation of vertiport lighting is to be in accordance with AC 150/5340-30, Design and Installation Details for Airport Visual Aids.

Table 4-1: Perimeter Lighting Intensity and Distribution
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=2>Approach Angle0 to 15 degrees</td><td rowspan=1 colspan=1>Approach Angle16 to 90 degrees</td></tr><tr><td rowspan=1 colspan=1>Color</td><td rowspan=1 colspan=1>Minimum</td><td rowspan=1 colspan=1>Minimum average intensity</td><td rowspan=1 colspan=1>Minimum</td></tr><tr><td rowspan=1 colspan=1>Green</td><td rowspan=1 colspan=1>10 cd</td><td rowspan=1 colspan=1>15 cd</td><td rowspan=1 colspan=1>5 cd</td></tr></table>

![55f2f189046e7a37ead75e9acd6fab9c5ef0b32dea125c8f81ba685218ed23e1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/55f2f189046e7a37ead75e9acd6fab9c5ef0b32dea125c8f81ba685218ed23e1.jpg)

## 4.5.2. In-Pavement Perimeter Lights on TLOF and FATO.

1. TLOF perimeter lights are green and FAA type L-861H (AC 150/5345-46) or FAA type L-852H. LED versions of FAA type L-861H and L-852H are per AC 150/5345- 46 and EB 67.

2. A square TLOF has:

a. One light in each corner.

b. Lights uniformly spaced between the corners with no less than five lights on each side including the corners.

c. Lights spaced no more than 25 feet (7.6 m) apart.

d. A light along the centerline of the approach.

3. A circular TLOF has:

a. An even number of lights

b. Minimum of eight lights uniformly spaced.

4. TLOF lights are within 1 foot (0.3 m) inside or outside of the perimeter line.

5. FATO perimeter lights are optional.

6. If installed, FATO perimeter lights are green and FAA type L-861H (AC 150/5345- 46) or FAA type L-852H. LED versions of FAA type L-861H and L-852H are per AC 150/5345-46 and EB 67.

7. A square FATO has:

a. One light in each corner.

b. Lights uniformly spaced between the corners with no less than five lights on each side.

c. Lights spaced no more than 25 feet (7.6 m) apart.

d. A light along the centerline of the approach.

8. A circular FATO has:

a. An even number of lights

b. Minimum of 8 lights uniformly spaced.

9. FATO lights are within 1 foot (0.3 m) of the inside or outside of the perimeter line.

Figure 4-6: TLOF/FATO Lighting  
![000f362b79eddbf70abfb9efa69440ba797f88849c96c976ddeab556927c5ea2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/000f362b79eddbf70abfb9efa69440ba797f88849c96c976ddeab556927c5ea2.jpg)  
In-pavement lights are within 1 foot (0.3 m) of the inside or outside of the TLOF and FATO respective perimeters.  
Elevated lights are outside and within 10 feet (3 m) of TLOF and FATO respective perimeters.  
Exhibit is configured for 50-foot (15.2 m) TLOF.

Figure 4-7: Elevated Vertiport Configuration Example  
![4eac54a2ad5cbfb86bcaee62ec089b7f5574ef95bbeb4589cc03acb6bb8f7778.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4eac54a2ad5cbfb86bcaee62ec089b7f5574ef95bbeb4589cc03acb6bb8f7778.jpg)  
Note: See Figure 4-8 for safety net and lighting details.

Figure 4-8: Elevated FATO Perimeter Lighting  
![97fcb81400ce93312a7c553d71955ed469db0600aa32418203003d9e98c7bae0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/97fcb81400ce93312a7c553d71955ed469db0600aa32418203003d9e98c7bae0.jpg)

Install either “A” Type L-852H, or “B” Type L-861H.

In-pavement edge light fixture Ⓐ (Type L-852H).

Omnidirectional light Ⓑ, mounted off the structure edge (Type L-861H).

Ensure elevated lights do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).

For TLOF and FATO lighting standards, see AC 150/5345-46 and EB 67.

A safety net’s supporting structure must be located below the safety net.

## 4.5.3. Elevated Perimeter Lights on TLOF and FATO.

The same standards for in-pavement lights apply to elevated lights except for the following:

1. Lights are omnidirectional.

2. Lights are on the outside edge of the TLOF and FATO.

3. Lights are on frangible elevated light fixtures, no more than 2 inches (51 mm) above the TLOF surface, and no more than 10 feet (3 m) out from the TLOF and FATO, respective, perimeters.

4. Lights do not penetrate a horizontal plane at the TLOF edge elevation by more than 2 inches (51 mm), as shown in Figure 2-3.

See additional information in Figure 4-6.

## 4.5.4. Visual Glideslope Indicators (VGSI).

A VGSI provides pilots with visual vertical course and descent cues. Install the VGSI such that the lowest on-course visual signal provides a minimum of one degree of clearance over any object that lies within ten degrees of the approach course centerline.

## 4.5.4.1. Siting.

1. The optimum location of a VGSI is on the extended centerline of the approach path at a distance that brings the VTOL to a hover with the undercarriage between 3 and 8 feet (0.9 to 2.4 m) above the TLOF.

2. To properly locate the VGSI, estimate the vertical distance from the undercarriage to the pilot’s eye.

## 4.5.4.2. Control of the VGSI.

Design the VGSI to be pilot controllable such that it is “on” only when needed as an option.

## 4.5.4.3. VGSI Needed.

A VGSI is an optional feature. However, install a VGSI if one or more of the following conditions exist, especially at night:

1. Obstacle clearance, noise abatement, or traffic control procedures necessitate a slope to be flown.

2. The environment of the VTOL provides few visual surface cues.

## 4.5.4.4. Additional Guidance.

Additional guidance is provided in AC 150/5345-52, Generic Visual Glideslope Indicators (GVGI), and AC 150/5345-28, Precision Approach Path Indicator (PAPI) Systems.

## 4.5.5. Approach Lighting.

Approach lights are optional. When installed they include a line of five green omnidirectional lights located on the centerline of the preferred approach/departure path. The first light is 30 to 60 feet (9.1 to 18.3 m) from the TLOF. Remaining lights are spaced at 15-foot (4.6 m) intervals aligned on the centerline of the approach path. See Figure 4-6.

## 4.5.6. Floodlight Option.

The FAA has not evaluated floodlights for effectiveness in visual acquisition of a vertiport. Guidelines for the use and installation of floodlights include:

1. Install floodlights to illuminate the TLOF, the FATO, and/or the parking area if ambient light does not suitably illuminate markings for night operations.

2. Mount these floodlights on adjacent buildings to eliminate the need for tall poles, if possible. Place floodlights clear of the TLOF, the FATO, the Safety Area, the approach/departure surfaces, and transitional surfaces and ensure floodlights and their associated hardware do not constitute an obstruction hazard.

3. Aim floodlights down to provide adequate illumination on the apron and parking surface.

4. Ensure floodlights that might interfere with pilot vision during takeoff and landings are capable of being turned off by pilot control or at pilot request.

Note 1: Floodlights do not replace TLOF or FATO lighting recommendations.

Note 2: White lighting for heliport applications should not be activated until the aircraft has landed and deactivated prior to takeoff.

## 4.6. Identification Beacon.

An identification beacon, FAA type L-801H Medium intensity heliport beacon, is required for night operations. The identification beacon is flashing white/yellow/green with a rate of 30 to 45 flashes per minute. On-airport vertiports are not required to have a vertiport identification beacon. Install beacons per the heliport guidance below:

1. AC 150/5345-12, Specification for Airport and Heliport Beacons, provides specifications for a beacon.

2. AC 150/5340-30 provides guidelines for installing a beacon.

## 4.7. Wind Cone.

Wind cones provide the direction and magnitude of the wind. The following guidelines apply to wind cones:

1. Minimum of one wind cone conforming to AC 150/5345-27, FAA Specification for Wind Cone Assemblies.

2. Orange in color to provide the best possible contrast to its location’s background.

3. Locate to provide valid wind direction and speed information near the vertiport under all wind conditions.

4. Visible to pilots on the approach path when the aircraft is 500 feet (152 m) from the TLOF.

5. Visible to pilots from the TLOF.

6. Located within 500 feet (152 m) horizontal of the TLOF.

7. If one location does not provide for all the above, multiple locations may be necessary to provide pilots with all the wind information needed for safe operations.

8. See AC 150/5345-27 and AC 150/5340-30 for primary and secondary wind cones for multiple wind cone requirements.

9. Located outside the Safety Area and does not penetrate the approach/departure or transitional surfaces.

10. Follows installation details specified in AC 150/5340-30.

11. Lighted internally or externally for night operations.

## 5.0 Charging and Electric Infrastructure.

Most early concepts of operation for AAM activity indicate the use of electric propulsion by VTOL aircraft. The electrical needs for these aircraft vary based on design and manufacturer. This EB addresses battery driven technologies. Future guidance will be provided on other emerging energy concepts (e.g., hydrogen).

Electrification of aviation propulsion systems is an evolving area with few industryspecific standards. In addition to relevant national, state, and local building codes, the following sections provide a partial list of relevant standards that may assist when specifying charging systems and facility layout for this emerging industry. Current charging standards for light duty vehicle charging (up to 350kw) align with multiple light electric aircraft currently applying for certification. However, for meeting operational characteristics of higher capacity batteries and novel systems, manufacturers and operators may implement, along with fixed-charger equipment, alternate charging methods including mobile charging systems, fixed battery storage, cable and/or on-board battery cooling, battery swapping, or other concepts.

At the time of this publication, consensus has not been achieved regarding classes of charging or connection standards and could vary based on the aircraft duty cycle, charging speed, battery chemistry, charging system, and battery cooling system, etc. Charging infrastructure design for vertiports should consider adapting to multiple aircraft specific systems. Additional guidance is currently being developed as the AAM industry continues to evolve. When siting charging stations and equipment, consider all potential safety hazards and guidance in the other sections of this EB.

Battery charging must be done in a safe and secure manner. Any aircraft batteries stored on site should be stored safely away from TLOF, FATO, and safety areas and not penetrate the approach/departure surfaces, and be in accordance with all applicable building codes, fire codes, and NFPA Standards. As additional research is developed, further recommendations will be released.

## 5.1. Standards.

5.1.1. Airport/Vertiport Fire Fighting and Safety Considerations.

2021 International Fire Code (IFC): To implement alternative energy vectors, there is the need for general precautions, emergency planning and preparedness, and storage of hazardous materials.

NFPA 110, Standard for Emergency and Standby Power Systems: To ensure the continuity of electric aircraft operations, uninterrupted power supply is needed thus creating a need for guidelines on emergency and backup power supply systems.

NFPA 70, NEC Article 625 - Electric Vehicle Charging System: Covers the electrical conductors and equipment external to an electric vehicle that connect an electric vehicle to a supply of electricity by conductive or inductive means, and the installation of equipment and devices related to electric vehicle charging. It also

addresses scenarios that would allow the use of load balancing functions on electrical supply systems.

NFPA 70, Article 706 - Energy Storage Systems: This article applies to all energy storage systems (ESS) having a capacity greater than 3.6 mJ (1 kWh) that may be standalone or interactive with other electric power production sources. These systems are primarily intended to store and provide energy during normal operating conditions.

NFPA 400, Hazardous Materials Code: Covers the minimum NFPA standards for the storage and handling of hazardous materials such as lithium batteries.

NFPA 415, Standard on Airport Terminal Buildings, Fueling Ramp Drainage, and Loading Walkways: The purpose of this standard is to protect life and property from fire at airport terminal complexes.

NFPA 418, Standard for Heliports and Vertiports: This standard establishes fire safety standards for operations of heliports and rooftop hangars for the protection of people, aircraft, and other property. Future editions of this standard will include electric mobility asset considerations.

NFPA 855, Standard for the Installation of Stationary Energy Storage Systems: Covers the minimum NFPA standards established for design, installation, and maintenance of a stationary energy storage system including battery storage systems.

## 5.1.2. Occupational Safety and Health Administration Considerations.

29 CFR § 1910.176, Handling Materials – General: This standard provides the minimum requirements for the storage and handling of hazardous materials such as lithium batteries.

## 5.1.3. Power Quality Considerations.

IEEE 519-2014, IEEE Recommended Practice and Requirements for Harmonic Control in Electric Power Systems: The grid impact of high wattage charging stations needs to be considered when designing and adopting charging stations. This standard provides guidance in the design and compliance of power systems with nonlinear loads.

IEEE 1826-2020, IEEE Standard for Power Electronics Open System Interfaces in Zonal Electrical Distribution Systems Rated Above 100 kW: Airports require power, monitoring, information exchange, control, and protection of interfaces that are based on technological maturity, accepted practices, and allowances for future technology insertions such as the integration of electric aircraft.

## 5.1.4. Underwriter’s Laboratories (UL) Certifications Considerations.

The following standards focuses on certifying the components and safety of the systems.

UL 2202, Standard for Safety of Electric Vehicle (EV) Charging System Equipment: Covers conducting charging system equipment (600 volts or less) for recharging batteries in surface electric vehicles.

UL 2251, Standard Testing for Charging Inlets and Plugs: Covers plugs, receptacles, vehicle inlets, and connectors rated up to 800 amperes and up to 600 volts AC or DC, and intended for conductive connection systems, for use with electric vehicles.

• UL 2580, Batteries for Use in Electric Vehicles: Covers electric equipment storage assemblies in electric powered vehicles.

UL 9540, Energy Storage System (ESS) Requirements - Evolving to Meet Industry and Regulatory Needs: This key standard encompasses the design, commissioning, operation, decommissioning, and emergency operations for all energy storage systems.

UL 9540a, Test Method.

## 5.1.5. Vehicle to Infrastructure Considerations.

SAE J1772, SAE Electric Vehicle and Plugin Hybrid Electric Vehicle Conductive Charge Coupler: This standard was developed to define the fit and function of a conductive coupler for use in charging electric vehicles. It was later expanded to include direct current (DC) charging through combined alternating current/direct current (AC/DC) physical connector referred to as the Combined Charging Standard (CCS).

SAE AIR7357, MegaWatt and Extreme Fast Charging for Aircraft (under development): This standard is a work in progress under SAE leadership and intended to provide a charging interface for battery packs from 150kWh-1MWh within aircraft.

Megawatt Charging System (MCS): The MCS is intended to extend the capabilities of the CCS to accommodate the charge rate demands of larger vehicles and thus serve the trucking and aviation sectors. Ratings should exceed 1MW (max 1,250 volt and 3,000 ampere (DC)) while also addressing communication and controls using ISO/IEC 15118-1:2019 and meeting UL 2251 touch safe standards.

ISO/IEC 15118-1:2019, Road Vehicles: Vehicle to Grid Communication Interface: This standard defines the digital communications protocol to be used for the charging of high voltage electric vehicle batteries from a charging station. Beyond the basic handshakes and charge control between a vehicle and a charging station, this standard also includes convenience and security layers that support the “plug and charge” experience. Additionally, it offers the potential to schedule and coordinate the charging demands with the grid conditions.

## 5.2. Other Information.

5.2.1. National Renewable Energy Laboratory (NREL) Federal Aviation Administration Vertiport Electrical Infrastructure Study. With the introduction of eVTOL aircraft, electrical charging loads will be added at the vertiports along with building loads and distributed energy resources (DERs). The key research challenge is the optimization of megawatt-scale building loads, charging loads, energy storage, and renewables production. To better understand vertiport infrastructure requirements, the FAA identified multiple stakeholders in the Report including aircraft manufacturers, electric utilities, potential site property owners, and local communities to evaluate their unique operational needs.

5.2.2. NREL Overview of Potential Hazards in Electric Aircraft Charging Infrastructure. The objective of this Report is to document and help familiarize the FAA and airport authorities with the potential hazards associated with the deployment of electric aircraft and the associated charging infrastructure. The list and examples of these hazards are non-exhaustive, and multiple hazards can occur simultaneously. This Report discusses natural, human, and technological causes that can lead to fire (thermal), physical, or chemical hazards. Applicable standards and guidelines associated with electric vehicle supply equipment (EVSE) infrastructure are available for reference in the appendix. These sources, which address diverse geographic location and climate considerations, can help operators in site selection for EVSE, mitigation planning, deployment considerations, and training of staff to handle these situations.

5.2.3. NREL Addressing Electric Aviation Infrastructure Cybersecurity Implementation. This Technical Report evaluates key considerations of cybersecurity systems in preparation for the electrification of both legacy and new aviation services. The objectives are to consider the landscape of components and interconnections, review sensitivities and the criticality of operational data, consider applicability of existing best practices, and identify gaps associated with the cybersecurity of electric charging systems for the aviation sector. It is noted that cybersecurity analysis is a key component of the overall hazard analysis for aviation electrical infrastructure necessary for safely providing energy to aircraft.

## 6.0 On-Airport Vertiports.

To support VTOL operations, certain OEMs and operators are interested in developing vertiports on airports and modifying existing on-airport helicopter landing facilities. All federally obligated airport sponsors are required to ensure the safety, efficiency, and utility of the airport and to provide reasonable and not unjustly discriminatory access to all aeronautical users.

This chapter addresses design considerations for separate vertiport facilities on airports. There may be locations on an airport where VTOLs can operate without interfering with airplane traffic and operations. Operations can occur on existing airport infrastructure for its intended purpose or on dedicated vertiport facilities.

Separate vertiport facilities and approach/departure procedures may be needed when the volume of airplane and/or VTOL traffic affects operations. Airports with interconnecting passenger traffic between VTOLs and fixed-wing aircraft should generally provide access between the respective terminals for boarding with applicable security measures in place.

Any new vertiport infrastructure or fixed equipment must be depicted on the ALP and submitted for FAA review prior to development and operation. For projects subject to FAA approval, an appropriate level of environmental review under the National Environmental Policy Act (NEPA) is required. These on-airport vertiport facilities must follow all guidance detailed in this EB.

For facilities being built on non-federally obligated airports, in compliance with Part 157, the sponsor or proponent must submit Form 7480-1 at least 90 days in advance of the day that construction work is to begin on the vertiport takeoff and landing area.

See Appendix A for air traffic considerations for siting vertiports on or near existing airports.

## 6.1. On-Airport Location of TLOF.

Locate the TLOF to provide ready access to the airport terminal with applicable security measures in place or to the VTOL user’s origin or destination. If needed, locate the TLOF away from, but with access to, fixed-wing aircraft movement areas (the runways, taxiways, and other areas of an airport that are used for taxiing, takeoff, and landing of aircraft, exclusive of loading ramps and aircraft parking areas).

## 6.2. On-Airport Location of FATO.

See Table 6-1 for standards of the distance between the centerline of an approach to a runway and the centerline of an approach to a vertiport’s FATO for simultaneous, samedirection VFR operations. Figure 6-1 depicts an example of an on-airport Vertiport location. The FATO should be located outside of all object free areas (OFAs), Safety Areas, runway protection zones, and safety critical navigational aid areas, as defined in AC 150/5300-13, Airport Design.

Table 6-1: Recommended Minimum Distance between Vertiport FATO Center to Runway Centerline for VFR Operations
<table><tr><td rowspan=1 colspan=1>ReferenceVTOL AircraftMTOW</td><td rowspan=1 colspan=1>Airplane Size</td><td rowspan=1 colspan=1>Distance FromVertiport FATO Centerto Runway Centerline</td></tr><tr><td rowspan=1 colspan=1>12,500 1bs (5,670kg) or less</td><td rowspan=1 colspan=1>Small Airplane (12,500 1bs (5,670 kg) or less))</td><td rowspan=1 colspan=1>500 feet (152 m)</td></tr><tr><td rowspan=1 colspan=1>12,500 1bs (5,670kg) or less</td><td rowspan=1 colspan=1>Large Airplane (12,501-300,000 1bs (5,670.4-136,079 kg))</td><td rowspan=1 colspan=1>500 feet (152 m)</td></tr><tr><td rowspan=1 colspan=1>12,500 1bs (5,670kg) or less</td><td rowspan=1 colspan=1>Heavy Airplane (Over 300,000 1bs (136,079 kg))</td><td rowspan=1 colspan=1>700 feet (213 m)</td></tr></table>

Figure 6-1: Example of an On-airport Vertiport  
![c62940296887aafc0547e756169dbb9599d4d4dfbf78de8632b6cbc9665b4506.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c62940296887aafc0547e756169dbb9599d4d4dfbf78de8632b6cbc9665b4506.jpg)  
Note: See Table 6-1.  
Note: Figure does not reflect every type of configuration.

## 7.0 Site Safety Elements.

## 7.1. Fire Fighting Considerations.

Refer to NFPA 418, Standard for Heliports and Vertiports, for the most current guidance on fire protection. Refer to NFPA 855, Standard for the Installation of Stationary Energy Storage Systems, for guidance on safety standards for stationary and mobile energy storage systems. Chapters on emergency response provide relevant guidance for fire protection engineers, system designers, code officials, and emergency responders.

## 7.2. Security and Safety.

For vertiports located in secured airport environments, unless screening was carried out at the VTOL passengers’ departure location, Transportation Security Administration regulations may require that a screening area and/or screening be provided before passengers enter the airport’s secured areas. If necessary, airports should establish multiple VTOL parking positions and/or locations in the terminal area to service VTOL passenger screening and/or cargo needs. General information about passenger screening is available on the Transportation Security Administration website, https://www.tsa.gov/.

Controlling vertiport access and keeping operational areas clear of people, animals, equipment, debris, and vehicles is important for safety and security. The following guidance applies to safety barriers and access control measures:

1. For ground-level vertiports, erect a safety barrier around the VTOL aircraft operational areas in the form of a fence or a wall outside of the Safety Area and below the 8:1 elevation of the approach/departure surface. Other types of safety barriers may be used if they provide adequate positive deterrent to persons inadvertently entering an operational area and do not attract wildlife or negatively impact safety.

2. If necessary, near the approach/departure paths, install the barrier by placing it well outside the outer perimeter of the Safety Area and below the elevation of the approach/departure and transitional surfaces described in paragraph 2.5.

3. Safety barriers must be high enough to present a positive deterrent to persons inadvertently or maliciously entering an operational area, but at a low enough elevation to be non-hazardous to all aircraft operations.

4. Provide control access to airport airside areas with adequate security measures as required or recommended by the Transportation Security Administration.

5. Display a vertiport caution sign like that shown in Figure 6-2 at all vertiport access points.

6. Ensure all persons are outside of the DCA when aircraft are operating, as described in paragraph 2.5.

For on-airport vertiports, proponents coordinates with their local Transportation Security Administration security representative.

# CAUTION VERTIPORT LANDING AREA

![327fc073f468faa1ce7ba3161e2ad76fd9588b4ac618ad80e73c07c8ae6a4fc1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/327fc073f468faa1ce7ba3161e2ad76fd9588b4ac618ad80e73c07c8ae6a4fc1.jpg)

AUTHORIZED PERSONNEL ONLY

## 7.3. Wind and Turbulence.

Wind conditions affect all aircraft to some degree. A wind analysis is recommended to determine the primary approach path to the vertiport. The FAA recommends a data period covering at least the last ten consecutive years of wind observations for this analysis.

Additionally, air (e.g., wind) flowing around and over buildings, stands of trees, terrain irregularities, and elsewhere can create turbulence on ground-level and rooftop vertiports that may affect VTOL operations. The following guidelines apply to turbulence:

1. When possible, locate the TLOF away from buildings, trees, and terrain to minimize air turbulence near the FATO and the approach/departure paths.

2. Assess the turbulence and airflow characteristics near and across the surface of the FATO to determine if turbulence mitigating design measures are necessary (e.g., air gap between the roof, roof parapet, or supporting structure). Perform this assessment when the FATO is located near the edge and top of a building or structure, or within the influence of turbulent wakes from other buildings or structures. The FAA’s

Technical Report FAA/RD-84/25, Evaluating Wind Flow around Buildings on Heliport Placement, addresses the wind’s effect on helicopter operations.

3. Providing a minimum 6-foot (1.8 m) unobstructed air gap on all sides above the level of the top of a structure (e.g., roof and adjacent parapets and walls) and the elevated vertiport will reduce the turbulent effect of air flowing over it.

4. Where an air gap or other turbulence-mitigating design measures are not taken on elevated structures, operational limitations may be necessary under certain wind conditions.

5. Airflow and turbulence measuring equipment may be required for rooftop vertiports. The airflow around the vertiport will need to be assessed to determine how many airflow measurement devices may be needed to accurately characterize the airflow

## 7.4. Weather Information.

An optional automated weather observing system (AWOS) measures and automatically broadcasts current weather conditions at the vertiport site. When installing an AWOS, locate it at least 100 feet (30.5 m) and not more than 700 feet (213 m) from the TLOF and such that its instruments will not be affected by rotor/propeller wash from VTOL operations. Find guidance on AWOS systems in AC 150/5220-16, Automated Weather Observing Systems (AWOS) for Non-Federal Applications, and FAA Order 6560.20, Siting Criteria for Automated Weather Observing Systems (AWOS). Other weather observing systems will have different siting criteria. Further research is being conducted as other systems may be able to provide weather data.

## 7.5. Winter Operations.

Swirling snow dispersed by a VTOL’s rotor/propeller wash can cause the pilot to lose sight of the intended landing point and/or obscure objects that need to be avoided. Elevated vertiports may benefit from the incorporation of in-surface snow and ice melt systems.

1. Design the vertiport to accommodate the methods and equipment to be used for snow removal.

2. Design the vertiport to allow the snow to be removed sufficiently so it will not present an obstruction hazard or a flying debris hazard to persons and vehicles.

3. For vertiports in winter weather, an optional dark TLOF surface can be used to absorb more heat from the sun and melt residual ice and snow.

4. Find guidance on winter operations in AC 150/5200-30, Airport Field Condition Assessments and Winter Operations Safety.

## 7.6. Access to Vertiports by Individuals with Disabilities.

Congress has passed various laws concerning access to airports. Since vertiports are a type of airport, these laws are similarly applicable. Find guidance in AC 150/5360-14, Access to Airports by Individuals with Disabilities.

## 7.7. Electromagnetic Effects.

Nearby electromagnetic devices, such as a large ventilator motor, elevator motor, magnetic resonance imaging machine (MRI), or other devices that consume large amounts of electricity may cause temporary abnormalities in the VTOL magnetic compass and interfere with other onboard navigational equipment. Buried rebar or other objects made of iron/steel below the vertiport surface have also been shown to interfere with a VTOL’s navigation instruments.

Be alert to the location of any such devices with respect to hospitals. A warning sign alerting pilots to the presence of an MRI is recommended. Take steps to inform pilots of the MRI locations or other electromagnetic equipment that consume large amounts of electricity. Vertiports are recommended to include electromagnetic interference (EMI) hazard marking and signage to alert pilots to potential EMI impacts, as shown in Figure 6-2 and Figure 6-3. Locate the EMI hazard sign at ingress/egress points on the vertiport for maximum visibility.

For additional information, see the FAA’s Technical Report FAA/RD-92/15, Potential Hazards of Magnetic Resonance Imagers to Emergency Medical Service Helicopter Services.

Figure 6-3. Vertiport EMI Hazard Marking  
![aea177d1876b0c6d9c8d0037c90ee56e866202065185080e11f8e596ebd00c91.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/aea177d1876b0c6d9c8d0037c90ee56e866202065185080e11f8e596ebd00c91.jpg)

Align the compass with magnetic north. Use arrows, as shown, to indicate the four cardinal headings (N, S, E, W) and four intercardinal headings (NE, SE, SW, and NW).

Use a minimum dimension of a 6-foot (1.8 m) outer diameter and a 4-foot (1.2 m) inner diameter for the compass circle.

Use blue paint for the compass circle and white paint for the inner portion of the compass. If necessary for visual contrast, use a one-foot white outline along the outer edge of the compass and arrows.

Figure 7-1. Vertiport EMI Hazard Sign

CAUTION

![cce1e59f8db27052a6d91fd2bfc96e958d2cfa07f9e7a9eb520c33f11f4a344c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/cce1e59f8db27052a6d91fd2bfc96e958d2cfa07f9e7a9eb520c33f11f4a344c.jpg)

Strong Magnetic Field

Aircraft navigational

instruments may be affected.

Confirm accuracy

of navigation instruments

during all operations.

# APPENDIX A. AIR TRAFFIC CONSIDERATIONS FOR SITING VERTIPORTS ON OR NEAR EXISTING AIRPORTS

The siting of vertiports supporting Advanced Air Mobility (AAM) aircraft capable of vertical takeoff and landing (VTOL) presents unique challenges. With the expected certification of AAM aircraft on the horizon and requests to establish vertiports already being received by the Federal Aviation Administration (FAA), additional guidance is needed.

Vertiport proponents should evaluate several factors when selecting potential sites. One important consideration is how current Air Traffic Control (ATC) procedures at a nearby airport may influence the capacity or efficiency of a proposed vertiport site. Adversely impacting these procedures could introduce safety issues, reduce capacity, and affect economic viability, especially when operating close to larger aircraft‡‡‡.

This guidance was developed to aid proponents in understanding key ATC considerations that may impact a proposed vertiport site serving AAM VTOL aircraft operating under visual flight rules (VFR). This document is not intended to replace or supersede official policy and guidance contained in Federal Regulations, FAA Orders, or facility Standard Operating Procedures. For detailed guidance, proponents should refer to the following resources:

1. FAA Order JO 7210.3, Facility Operation and Administration

2. FAA Order JO 7110.65, Air Traffic Control

## A.1. Definitions.

Below are definitions for various terms used throughout this appendix.

Visual Flight Rules (VFR): Rules that govern the procedures for conducting flight under visual conditions. The term “VFR” is also used in the United States to indicate weather conditions that are equal to or greater than minimum VFR requirements. In addition, it is used by pilots and controllers to indicate the type of flight plan.

Pilot or Controller Applied Visual Separation: a means used by ATC to separate aircraft in terminal areas and en route airspace in the NAS. There are two methods employed to accomplish this separation§§§:

1. The tower controller sees the aircraft involved and issues instructions, as necessary, to ensure that the aircraft avoid each other.

2. A pilot sees the other aircraft involved and upon instructions from the controller provides separation by maneuvering the aircraft to avoid it.

## A.2. Assumptions.

Applicable air traffic procedures and separation standards are determined by the type of aircraft (size, performance, wake category, etc.), flight rules (instrument flight rules (IFR) vs VFR), and class of airspace. This guidance assumes that the AAM VTOL aircraft using a proposed vertiport site will operate under VMC and VFR with an on-board pilot. In addition, pilot or controller applied visual separation will be utilized, when appropriate, to reduce operational impact.

## A.3. Air Traffic Considerations.

When selecting a vertiport site, it is advisable that vertiport proponents understand how the following air traffic considerations may impact the proposed vertiport operations. Failing to consider these in the site selection process may result in delays or restrictions on the proposed vertiport, reducing its operational efficiency.

## A.3.1. Impacts Due to Wake Turbulence Separation.

To avoid dangerous wake turbulence encounters, controllers apply appropriate wake turbulence separation between an airborne VTOL aircraft and larger aircraft\*\*\*\*. In general, the closer a vertiport FATO is to a runway, the more likely wake turbulence will impact its operations. As such:

1. A vertiport FATO located less than 700 feet (213 m) from the runway centerline may impact both runway and vertiport operations. At this distance, the effects of wake turbulence shall be mitigated for airborne VTOL aircraft during simultaneous operations with most aircraft. This proximity to a runway requires stringent operational coordination to prevent interference with aircraft taking off and landing.

2. A vertiport FATO located between 700 (213 m) and 2,499 feet (762 m) from a runway centerline may allow for more independent operations. Depending on aircraft type, flight directions, altitudes and other circumstances, wake turbulence mitigation may impact vertiport capacity and careful planning is still necessary to manage potential interactions with runway traffic.

3. A vertiport FATO located 2,500 feet (762 m) or more from a runway centerline has the greatest potential for independent flight paths and minimal disruption to runway operations. This separation enhances both safety and operational efficiency.

In addition to lateral separation, vertical separation is also critical. VTOL aircraft operating VFR must be able to enter their vertiport ingress/egress routes at an altitude at least 500 feet (152 m) above/below aircraft arriving or departing from the runway. If the VTOL is following or passing underneath a heavy/super aircraft, a minimum of 1,000 feet separation is required.

## A.3.2. Impacts Due to Missed Approach Procedures for Fixed-Wing Aircraft.

Many airports have instrument approach procedures to safely guide aircraft to land when cloud ceilings or visibility are reduced. One important component of an instrument approach procedure is the missed approach procedure. A missed approach procedure gives pilots instructions on how to proceed in case a safe landing cannot be continued.

When an aircraft is on final approach, ATC ensures that the missed approach procedure is clear of other traffic. At airports with a significant number of operations, this can cause additional delays to VTOL aircraft arriving or departing the vertiport.

## A.3.3. Impacts Due to Departure Procedures.

Existing Area Navigation (RNAV) instrument departures (or other departure procedures) allowing aircraft to fly headings that diverge from the runway centerline may limit arrival/departure flexibility from the vertiport and must be assessed on a site-specific basis.

## A.3.4. Impacts Due to Visual Flight Pattern.

Airports have established visual traffic patterns to better organize the flow of VFR aircraft arrivals and departures. These traffic patterns are typically 1,000 feet (305 m) above ground level (AGL) and can be on either side of a runway.

At airports with a significant number of VFR operations, the visual traffic pattern can become busy, with numerous aircraft in the pattern simultaneously. For this reason, a vertiport that is located below the visual traffic pattern may experience additional delays as controllers sequence VTOL arrivals and departures with aircraft in the visual traffic pattern.

## A.4. Vertiport Siting Scenarios.

This section illustrates how the air traffic consideration discussed above would apply to three common vertiport site scenarios. These scenarios are 1) vertiport located adjacent to a runway, 2) vertiport between parallel runways, and 3) vertiport off-the-end of a runway. The graphic below provides a graphical depiction of these scenarios.

## A.4.1. Vertiport Location Adjacent to Airport Runways.

When siting a vertiport adjacent to an airport runway, it is essential to consider the distance from the runway centerline. As discussed in the previous section, a vertiport FATO located closer than 2,500 feet (762 m) from the runway centerline could impact runway operations and incur vertiport delays.

Figure A-1. Siting Vertiports on or Near Existing Airports  
![bd2da66a3ef4d82af15a5a1e471b5eddc47a9359ce3beabd53a3fbfc0d8787ad.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/bd2da66a3ef4d82af15a5a1e471b5eddc47a9359ce3beabd53a3fbfc0d8787ad.jpg)  
Note: These notional depictions are not to scale and only illustrate the relative position of a vertiport in relation to a runway. The actual distances from the runway are critical to assessing the potential impacts.

Vertiport proponents should also be aware that VTOL aircraft crossing an active runway may be delayed by ATC until there is a sufficient gap between runway operations. As such, VTOL aircraft to/from destinations that are located on the other side of a runway at a busy airport may experience additional delays and/or circuitous routings.

Another important consideration is the vertiport location relative to the visual traffic pattern. A vertiport that is located below the visual traffic pattern may experience delays as controllers sequence VTOL arrivals and departures with aircraft in the traffic pattern.

Lastly, when siting a vertiport adjacent to an airport runway, vertiport proponents should become familiar with the missed approach procedures at the airport. If a vertiport is in the path of a missed approach procedure, controllers may need to apply additional buffer between an aircraft landing at the airport and VTOL aircraft landing/departing the vertiport.

## A.4.2. Vertiport Location Between Parallel Runways.

In addition to the considerations discussed in the previous section, vertiports located between parallel runways introduce additional ATC complexities that could increase delays for VTOL aircraft. With runways on both sides of the vertiport, ATC must consider multiple active flight paths, types of aircraft, and limitations.

When a VTOL aircraft arrives/departs a vertiport located between parallel runways, it must either fly over a runway or proceed parallel to the runway until it can safely cross the extended runway centerline. In some cases, the most direct route would be to fly over the runway. However, at busy airports, the efficiency impacts due to wake turbulence separation and/or missed approach procedures can create significant delays for VTOL aircraft. In other cases, arriving/departing parallel to the runways before crossing the extended runway centerline may result in less delay, but it could also increase flying time/distance.

## A.4.3. Vertiport Location Off the End of Airport Runways.

Vertiports located near the approach or departure end of an airport runway may present significant challenges for ATC. Locations closer to the runway arrival threshold or departure ends will present greater difficulty than those farther away and incur more delays and/or operational restrictions.

For example, if a vertiport is placed along the extended runway centerline, vertiport aircraft must be able to enter their ingress/egress routes at an altitude at least 500 feet (152 m) below traffic arriving or departing from the runway (1,000 feet when passing underneath a heavy/super aircraft). If the vertiport is close enough to the runway and the above separation cannot be achieved, VTOL operations will need to be delayed until there is a sufficient gap in the arrival or departure sequence to the runway.

## APPENDIX B. ACRONYMS AND TERMS

<table><tr><td>AAM</td><td>advanced air mobility</td></tr><tr><td>AC</td><td>Advisory Circular</td></tr><tr><td>AC</td><td>alternating current</td></tr><tr><td>ADA</td><td>Americans with Disabilities Act</td></tr><tr><td>ALP</td><td>Airport Layout Plan</td></tr><tr><td>AWOS</td><td>automated weather observing system</td></tr><tr><td>CCS</td><td>combined charging standard</td></tr><tr><td>CD</td><td>candela</td></tr><tr><td>CFR</td><td>Code of Federal Regulations</td></tr><tr><td>D</td><td>controlling dimension</td></tr><tr><td>DC</td><td>direct current</td></tr><tr><td>DCA</td><td>downwash/outwash caution area</td></tr><tr><td>DER</td><td>distributed energy resource</td></tr><tr><td>DWOW</td><td>Downwash/Outwash</td></tr><tr><td>EB</td><td>Engineering Brief</td></tr><tr><td>EMS</td><td>Emergency Medical Service</td></tr><tr><td>ESS</td><td>energy storage system</td></tr><tr><td>ETL</td><td>effective translational lift</td></tr><tr><td>EV</td><td>electric vehicle</td></tr><tr><td>EVSE</td><td>electric vehicle supply equipment</td></tr><tr><td>eVTOL</td><td>electric vertical takeoff and landing</td></tr><tr><td>FAA</td><td>Federal Aviation Administration</td></tr><tr><td>FATO</td><td>final approach and takeoff area</td></tr><tr><td>FC</td><td>failure condition</td></tr><tr><td>FOD</td><td>foreign object debris</td></tr><tr><td>GSE</td><td>ground service equipment</td></tr><tr><td>GVGI</td><td>generic visual glideslope indicators</td></tr><tr><td>HOGE</td><td>hover out of ground eff ect</td></tr><tr><td>IEC</td><td>International Electrotechnical Commission</td></tr><tr><td>IEEE</td><td>Institute of Electrical and Electronics Engineers</td></tr><tr><td>IFC</td><td>International Fire Code</td></tr><tr><td>IFR</td><td>instrument flight rules</td></tr><tr><td>IMC</td><td>instrument meteorological conditions</td></tr><tr><td>ISO</td><td>International Organization for Standardization</td></tr><tr><td>kph</td><td>kilometers per hour</td></tr><tr><td>kWh</td><td>kilowatt per hour</td></tr><tr><td>LAP</td><td>Landing Area Proposal</td></tr><tr><td>LBA</td><td>load-bearing area</td></tr><tr><td>LED</td><td>light emitting diode</td></tr><tr><td>LOB</td><td>line of business</td></tr><tr><td>MCS</td><td>megawatt charging system</td></tr><tr><td>mJ</td><td>millijoule</td></tr><tr><td>MSL</td><td>mean sea level</td></tr><tr><td>MTOW</td><td>maximum takeoff weight</td></tr><tr><td>MW</td><td>megawatt</td></tr><tr><td>MWh</td><td>megawatt per hour</td></tr><tr><td>NAS</td><td>National Airspace System</td></tr><tr><td>NEC</td><td>National Electric Code</td></tr><tr><td>NEPA</td><td>National Environmental Policy Act</td></tr><tr><td>NEMSPA</td><td>National EMS Pilots Association</td></tr><tr><td>NFPA</td><td>National Fire Protection Association</td></tr><tr><td>NREL</td><td>National Renewable Energy Laboratory</td></tr><tr><td>OEM</td><td>original equipment manufacturer</td></tr><tr><td>OFA</td><td>object free area</td></tr><tr><td>PAPI</td><td>precision approach path indicator</td></tr><tr><td>PPR</td><td>prior permission required</td></tr><tr><td>R&amp;D</td><td>Research and Development</td></tr><tr><td>RD</td><td>Rotor diameter</td></tr><tr><td>RNAV</td><td>Area Navigation</td></tr><tr><td>SAE</td><td>SAE International</td></tr><tr><td>TDPC</td><td>touchdown/positioning circle</td></tr><tr><td>TLOF</td><td>touchdown and liftoff area</td></tr><tr><td>UL</td><td>Underwriters Laboratories</td></tr><tr><td>VFR</td><td>visual flight rules</td></tr></table>

VGSI Visual Glideslope Indicator VMC visual meteorological conditions VTOL vertical takeoff and landing

# FAA AC 150/5390-2D Heliport Design

Subject: Heliport Design

Date: 1/5/2023

Initiated By: AAS-100

AC No: 150/5390-2D

Change:

1 Purpose.

This advisory circular (AC) provides standards for the planning, design and construction of heliports serving helicopters with single, tandem (front and rear) or dual (side by side) rotors.

2 Cancellation.

This AC cancels AC 150/5390-2C, Heliport Design, dated April 24, 2012.

3 Applicability.

The Federal Aviation Administration (FAA) recommends the standards and guidelines in this AC for uniformity in planning, design, and construction of heliports. This AC does not constitute a regulation, is not mandatory and is not legally binding in its own right. This AC will not be relied upon as a separate basis by the FAA for affirmative enforcement action or other administrative penalty. The standards and guidelines contained in this AC are practices the FAA recommends for establishing an acceptable level of safety, performance, and operation for heliports. Conformity with this AC is voluntary, except for the projects described in subparagraphs 1, 2, and 3 below:

Use of these standards and guidelines is mandatory for projects funded under Federal grant assistance programs, including but not limited to the Airport Improvement Program (AIP) and Coronavirus Aid, Relief, and Economic Security (CARES) Act Airport Grants program. See Grant Assurance #34. Heliport sponsors should familiarize themselves with the obligations and assurances that apply to each grant program from which they obtained grant funds.

This AC is mandatory, as required by regulation, for projects funded by the Passenger Facility Charge (PFC) program. See PFC Assurance #9.

This AC has no applicability under Title 14 Code of the Federal Regulations (CFR) Part 139 due to an exemption for heliport operators per § 139.1(c)(5).

Other federal agencies, states, or other authorities having jurisdiction over the construction of heliports not funded with AIP, CARES Act, or PFC funds have discretion in establishing the extent to which these standards apply.

## 4 Related Documents.

ACs and Orders referenced in the text of this AC do not include a revision letter, as they refer to the latest version. See Appendix E for a list of associated publications.

## 5 Principal Changes.

The AC incorporates the following principal changes:

Complete reorganization of this AC:

a. Consolidated Chapters 2, 3 and 4 (GENERAL AVIATION, TRANSPORT, and HOSPITAL heliport chapters, respectively) into Chapter 2.

b. Consolidated Chapter 7 (Heliport Gradients and Pavement Design) into Chapter 2.

c. Included a separate Chapter 3 on Heliport Taxiways, Taxi Routes, and Helicopter Parking.

d. Included a separate Chapter 4 on Heliport Markings and Lighting.

e. Included a separate Chapter 7 on Heliport Site Safety Elements.

f. Added new Appendix B, Pre-designated Emergency Landing Areas (PELAs).

g. Incorporated Engineering Brief #87, Heliport Perimeter Light for Visual Meteorological Conditions, into this AC to address specific heliport lighting requirements. Heliport lighting design requirements are included in Appendix G.

Revised figures and tables to correspond with the design requirements and dimensions for GENERAL AVIATION, TRANSPORT, and HOSPITAL heliports.

Enhanced the figures to include dimensional, layout, and offset requirements.

Updated the format of the document and made minor editorial changes throughout.

Included a heliport evaluation process flow chart in Appendix F.

## 6 Using this Document.

Hyperlinks (allowing the reader to access documents located on the internet and to maneuver within this document) are provided throughout this document and are identified with underlined text. When navigating within this document, return to the previously viewed page by pressing the “ALT” and “ ←” keys simultaneously.

Figures in this document are general representations and are not to scale. Colors and shading used in the figures are illustrative only. Guidance on specific heliport markings is provided in Chapter 4.

## 7 Use of Metrics.

Throughout this AC, U.S. customary units are used followed with “soft” (rounded) conversion to metric units. The U.S. customary units govern.

## 8 Where to Find this AC.

You can view a list of all ACs at

https://www.faa.gov/regulations\_policies/advisory\_circulars/. You can view the Federal Aviation Regulations at https://www.faa.gov/regulations\_policies/faa\_regulations/.

## 9 Feedback on this AC.

If you have suggestions for improving this AC, you may use the Advisory Circular Feedback form at the end of this AC.

![3ce1e07403a9d94d02e5bba6c045344fe9d723493352f76a0e2d7ed65cd5b904.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3ce1e07403a9d94d02e5bba6c045344fe9d723493352f76a0e2d7ed65cd5b904.jpg)

John R. Dermody

Director of Airport Safety and Standards

## CONTENTS

Paragraph Page   
CHAPTER 1. Introduction.. .... 1-1   
1.1 Background.. ..... 1-1   
1.2 General... .... 1-1   
1.3 Facilities. . .... 1-1   
1.4 Planning. ... .... 1-2   
1.5 Existing Heliports. ..... ..... 1-2   
1.6 Location. ............. ...................... 1-2   
1.7 AC Organization. ........ ....... 1-3   
1.8 Explanation of Terms...... ....... 1-3   
1.9 Selection of Approach/Departure Paths.. ... 1-10   
1.10 Notification Requirements. .. ..... 1-10   
1.11 Hazards to Air Navigation. . .... 1-15   
1.12 Federal Assistance. . ... 1-18   
1.13 Environmental Impact Analyses.. ... 1-18   
1.14 Terminal Facilities Design Considerations.. ..... 1-19   
1.15 Zoning for Compatible Land Use. ...... ................. 1-19   
1.16 Access to Heliports by Individuals with Disabilities..... ....... 1-20   
1.17 State Role. ... ..... 1-20   
1.18 Local Role and Building Code.. ... 1-20   
1.19 Related Referenced Material.. .... 1-20   
CHAPTER 2. Heliport Design... ..... 2-1   
2.1 General... .... 2-1   
2.2 Prior Permission Required (PPR) Facilities........... ........ 2-1   
2.3 Design Approach. ..... .... 2-1   
2.4 Access by Individuals with Disabilities.. ..... 2-1   
2.5 Heliport Site Selection. . ... 2-4   
2.6 TLOF/FATO and Safety Area Relationships. ..... 2-7   
2.7 Touchdown and Liftoff Area (TLOF).. ... 2-9   
2.8 Final Approach and Takeoff Area (FATO). .. 2-17

## CONTENTS

Paragraph Page   
2.9 Safety Area.. .. 2-21   
2.10 Fall Protection and Safety Net Design.. ... 2-24   
2.11 Pavement Design and Soil Stabilization. . ... 2-25   
2.12 VFR Approach/Departure Paths. . .. 2-27   
2.13 Heliport Protection Zone (HPZ). . .. 2-35   
2.14 Wind Cone. . ... 2-35   
CHAPTER 3. Heliport Taxiways, Taxi Routes, and Helicopter Parking ...... ...... 3-1   
3.1 General.. .... 3-1   
3.2 Taxiways and Taxi Routes....... ........ 3-1   
3.3 Taxiway/Taxi Route Widths..... ...... 3-1   
3.4 Taxiway Surfaces.... ..... 3-6   
3.5 Taxiway and Taxi Route Gradients. ... 3-6   
3.6 Helicopter Parking. . .... 3-6   
3.7 Parking Position Sizes.... .... 3-13   
3.8 Walkways.... ... 3-16   
3.9 Fueling. ........ ... 3-16   
3.10 Tiedowns.... ... 3-16   
CHAPTER 4. Heliport Markings and Lighting...... ......... 4-1   
4.1 General.. .... 4-1   
4.2 Heliport Retroreflective Markers and Markings. .... 4-1   
4.3 Standard Heliport Identification Marking... ..... 4-1   
4.4 TLOF and FATO Markings.. ..... 4-6   
4.5 Extended Pavement/Structure Markings for GENERAL AVIATION and   
HOSPITAL Heliports. ..... .... 4-10   
4.6 FATO Perimeter Markings. .... ................ ..... 4-10   
4.7 Flight Path Alignment Guidance Marking.. ... 4-11   
4.8 Taxiway and Taxi Route Markings..... ........................................................... 4-12   
4.9 Helicopter Parking Position Markings.. ...... 4-13   
4.10 Walkways..... ... 4-14   
4.11 Closed Heliport. . .. 4-14

## CONTENTS

Paragraph Page   
4.12 Marking Sizes. .. ... 4-15   
4.13 Heliport Lighting. . .. 4-15   
CHAPTER 5. Helicopter Facilities on Airports... ..... 5-1   
5.1 General.. .... 5-1   
5.2 Touchdown and Liftoff Area (TLOF). ... 5-1   
5.3 On-Airport Location of Final Approach and Takeoff Area (FATO). ... 5-1   
5.4 Safety Area..... ...... 5-3   
5.5 VFR Approach/Departure Paths. .. .... 5-3   
5.6 Heliport Protection Zone (HPZ). ... 5-3   
5.7 Taxiways and Taxi Routes..... ... 5-3   
5.8 Helicopter Parking. . .. 5-4   
5.9 Security. .. .. 5-4   
CHAPTER 6. Instrument Operations .... ..... 6-1   
6.1 General.. ... 6-1   
6.2 Planning. ... ... 6-3   
6.3 Airspace. .. ... 6-3   
6.4 Final Approach Reference Area (FARA). .. ...... 6-3   
6.5 Improved Instrument Lighting System. ... ..... 6-4   
6.6 Obstacle Evaluation Surfaces. .... 6-8   
6.7 Visual Glideslope Indicators (VGSI)... ..... 6-8   
CHAPTER 7. Heliport Site Safety Elements ... ..... 7-1   
7.1 General.... ..... 7-1   
7.2 Marking and Lighting of Difficult-To-See Objects.. ..... 7-1   
7.3 Safety Considerations. . ... 7-4   
Appendix A. Emergency Helicopter Landing Facilities (EHLF)..... ..... A-1   
A.1 General... .. A-1   
A.2 Notification and Coordination. .. ... A-1   
A.3 Rooftop Emergency Facilities.. .. A-1

## CONTENTS

Paragraph Page   
Appendix B. Pre-designated Emergency Landing Areas (PELAs) ..... ..B-1   
Appendix C. Helicopter Data... .... C-1   
Appendix D. Dimensions for Marking Size and Weight Limitations............... . D-1   
Appendix E. Associated Publications and Resources ...... .....E-1   
Appendix F. Heliport Evaluation Process Flow Chart ... .....F-1   
Appendix G. Design Requirements for Heliport Perimeter Lighting ..... ..... G-1   
G.1 Elevated and In-pavement Omnidirectional Helipad Perimeter Light. ... G-1   
G.2 Photometric Requirements.. .. G-2   
G.3 Additional Heliport Perimeter Light Requirements.. .. G-2   
G.4 L-860H and L-852H Light Fixture Testing. ... .. G-3   
G.5 Installation Criteria. .. .. G-3

## FIGURES

Figure 1-1. FAA Form 7480-1, Notice for Construction, Alteration and Deactivation of Airports   
... 1-12   
Figure 1-2. Example of a Heliport Layout Plan.. .... 1-13   
Figure 1-3. Example of a Heliport Location Map... ..... 1-14   
Figure 1-4. Offsite Development Requiring Notice to the FAA . ... 1-17   
Figure 2-1. GENERAL AVIATION Heliport – Basic Features... ... 2-2   
Figure 2-2. TRANSPORT Heliport – Basic Features...... ..... 2-3   
Figure 2-3. HOSPITAL Heliport (Ground Level) – Basic Features.. .. 2-4   
Figure 2-4. Heliport EMI Hazard Marking.. .. 2-6   
Figure 2-5. Heliport EMI Hazard Sign .... .. 2-7   
Figure 2-6. TLOF/FATO/Safety Area Relationships and Minimum Dimensions . .. 2-8   
Figure 2-7. Heliport Gradients and Rapid Runoff Shoulder - Load-bearing FATOs. ... 2-12   
Figure 2-8. Optional Elongated TLOF and FATO with Two Takeoff Positions.. ... 2-13   
Figure 2-9. Elevated Heliport: GENERAL AVIATION and HOSPITAL. ... 2-15   
Figure 2-10. Elevated Heliport: TRANSPORT . .... 2-16   
Figure 2-11. Additional FATO Length for Heliports at Higher Elevations .. ... 2-19   
Figure 2-12. Non-load-bearing FATO and Safety Area over Water: GENERAL AVIATION and   
HOSPITAL Heliports .. ... 2-23   
Figure 2-13. Non-load-bearing Safety Area over Water: TRANSPORT ... ... 2-24   
Figure 2-14. Helicopter Landing Gear Loading: Gradients and Pavement ..... ..... 2-26   
Figure 2-15. VFR Heliport Approach/Departure and Transitional Surfaces. .. 2-28   
Figure 2-16. VFR Curved Approach/Departure and Transitional Surfaces – GENERAL   
AVIATION and TRANSPORT Heliports. .. 2-29   
Figure 2-17. VFR HOSPTIAL and PPR Heliport Optional Lateral Extensions of the 8:1   
Approach/Departure Surface .. 2-31   
Figure 2-18. VFR HOSPITAL and PPR Heliport Optional Lateral Extension of the Curved 8:1   
Approach/Departure Surface . ... 2-33   
Figure 2-19. Flight Path Alignment Marking and Lights ... ... 2-34   
Figure 2-20. Heliport Protection Zone (HPZ).. ... 2-36   
Figure 3-1. Taxiway/Taxi Route Relationship – Paved Taxiway.. .. 3-2   
Figure 3-2. Taxiway/Taxi Route Relationship – Unpaved Taxiway with Elevated Retroreflective   
Edge Markers .... .. 3-3   
Figure 3-3. Taxiway/Taxi Route Relationship – Unpaved Taxiway with In-Pavement   
Retroreflective Edge Markers ........ ...... 3-4   
Figure 3-4. Hover Taxi Area.. ... 3-5   
Figure 3-5. Typical Parking Area Design – “Taxi-through” Parking Positions. ............ ........ 3-7   
Figure 3-6. Typical Parking Area Design – “Turn-around” Parking Positions ....... ...... 3-8   
Figure 3-7. Typical Parking Area Design – “Back-out” Parking Positions.. .... 3-9   
Figure 3-8. “Turn-around” Parking Position Marking.. .. 3-11   
Figure 3-9. “Taxi-through” and “Back-out” Parking Position Marking.. .. 3-12   
Figure 3-10. Parking Position Identification, Size, and Weight Limitations – Paved Areas, Turn-  
Around Parking...... ..... 3-14   
Figure 3-11. Parking Position Identification, Size, and Weight Limitations – Paved Areas, “Taxi  
through” and “Back-out” Parking........ ........ 3-15   
Figure 4-1. Standard TLOF Markings ..... .... 4-3   
Figure 4-2. Standard Heliport Identification Symbol, TLOF Size and Weight Limitations ....... 4-4   
Figure 4-3. HOSPITAL Heliport – Standard Identification Marking.. .... 4-5   
Figure 4-4. HOSPITAL Heliport – Alternative Identification Marking.. .... 4-6   
Figure 4-5. Paved TLOF/Paved FATO – Paved TLOF/Unpaved FATO – Marking:   
TRANSPORT Heliports and Other Heliports with a Paved TLOF...... ...... 4-7   
Figure 4-6. Unpaved TLOF/Unpaved FATO – Marking: GENERAL AVIATION and   
HOSPITAL Heliports ... .... 4-8   
Figure 4-7. Extended Pavement/Structure Marking: GENERAL AVIATION and HOSPITAL   
Heliports.. ... 4-11   
Figure 4-8. Marking a Closed Heliport... ................................... ...... 4-15   
Figure 4-9. Elevated TLOF – Perimeter Lighting ...... .................................. ..... ...... 4-17   
Figure 4-10. TLOF/FATO Perimeter Lighting...... ................ .... 4-18   
Figure 4-11. TLOF In-pavement and FATO Elevated Perimeter Lighting . .... 4-19   
Figure 4-12. FATO Elevation.. .... 4-21   
Figure 4-13. Landing Direction Lights. .. 4-23   
Figure 5-1. Example of Heliport Facilities Located on an Airport.. .. 5-2   
Figure 6-1. FARA/FATO Relationship: Precision Instrument Procedure...... ....... 6-4   
Figure 6-2. Heliport Instrument Lighting System (HILS): Non-precision .... ....... 6-6   
Figure 6-3. Heliport Approach Lighting System ... ....... 6-7   
Figure 6-4. Visual Glideslope Indicator (VGSI) Siting and Clearance Criteria .......................... 6-9   
Figure 7-1. Airspace Where Heliport Marking and Lighting are Recommended: Straight   
Approach.. ... 7-2   
Figure 7-2. Airspace Where Heliport Marking and Lighting are Recommended: Curved   
Approach.. .. 7-3   
Figure 7-3. Heliport Caution Sign . .. 7-5   
Figure A-1. Rooftop Emergency Landing Facility.. . A-2   
Figure C-1. Helicopter Dimensions ... . C-2   
Figure D-1. Form and Proportions of 36-inch (0.9 m) Numbers for Marking Size and Weight   
Limitations . . D-2   
Figure D-2. Form and Proportions of 18-inch (0.5 m) Numbers for Marking Size and Weight   
Limitation. . D-3   
Figure G-1. Perimeter Light Intensity Distribution ... . G-2

## TABLES

Table 2-1. TLOF/FATO Minimum Dimensions 1 .. 2-8   
Table 2-2. Minimum Dimensions for Elongated FATO with Two Takeoff Positions.... .. 2-13   
Table 2-3. TLOF Elevation and Configuration of Rooftop and other Elevated Heliports ........ 2-14   
Table 2-4. Minimum VFR Safety Area Width as a Function of Heliport Markings GENERAL   
AVIATION, HOSPITAL, and PPR Heliports... ... 2-21   
Table 2-5. Differences in Safety Net Design for Rooftop and Elevated Heliports.. .. 2-25   
Table 3-1. Taxiway/Taxi Route Dimensions – GENERAL AVIATION, TRANSPORT, and   
HOSPITAL Heliports .. .. 3-5   
Table 4-1. FATO Perimeter Light Design .. ... 4-20   
Table 5-1. Recommended Distance between FATO Center to Runway Centerline for VFR   
Operations .. .. 5-3   
Table 6-1. Standards for Instrument Approach Procedures. .. 6-2   
Table C-1. Helicopter Data . . C-3   
Table G-1. Helicopter Approach Angles Assuming VMC. . G-1   
Table G-2. Perimeter Lighting Intensity Recommendations .. . G-2

# CHAPTER 1. Introduction

## 1.1 Background.

Section 103 of the Federal Aviation Act of 1958 states in part, “In the exercise and performance of his power and duties under this Act, the Secretary of Transportation shall consider the following, among other things, as being in the public interest: (a) The regulation of air commerce in such manner as to best promote its development and safety and fulfill the requirements of defense; (b) The promotion, encouragement, and development of civil aeronautics . . .” This public charge, in effect, requires the development and maintenance of a national system of safe heliports. Using the standards and recommendations contained in this publication in the design of heliports supports this public charge.

These standards and recommendations do not limit or regulate the operations of helicopters, aircraft or heliports. When it is not feasible to meet the standards and recommendations in this advisory circular (AC), consult with the appropriate offices of the Federal Aviation Administration (FAA) Office of Airports and Flight Standards Service to identify possible adjustments to include operational procedures that accommodate safe heliport operations to the maximum extent.

The guidance provided in this AC is limited to heliports and helicopter operations. This AC does not specifically consider the characteristics of all vertical takeoff and landing (VTOL) aircraft or unmanned aircraft. New aircraft entrants that have an interest in operating at heliports should work with the FAA Office of Airports and Flight Standards to demonstrate that their aircraft’s operational and safety parameters comply with this AC, prior to operations.

The FAA is developing guidance for vertiports that would be intended for VTOL and/or unmanned aircraft. Until that guidance is published, entities developing operating sites for new aircraft entrants are encouraged to work with the FAA Office of Airports and Flight Standards on applicable design, operational, and safety criteria tailored to the performance of aircraft which intend to operate at those facilities.

## 1.2 General.

This chapter provides:

an explanation of terms used in this AC,

• notification responsibilities of heliport proponents to the FAA,

general heliport siting guidance, and

sources of technical information relating to the planning and design of a civil heliport.

## 1.3 Facilities.

Most heliports are not large and elaborate. A minimal facility may be adequate as a private-use prior permission required (PPR) heliport (see Appendix A) and may serve as the initial phase in the development of a public-use heliport capable of serving the

general aviation segment of the helicopter community. See Chapter 2 for requirements and design guidance for each specific heliport type.

The basic elements of a heliport include:

clear approach/departure paths,

• clear area for ground maneuvers,

• final approach and takeoff area (FATO),

• touchdown and liftoff area (TLOF),

safety area, and

a wind cone.

## 1.4 Planning.

This AC is a design document intended to assist engineers, architects, and city planners to design, locate, and build a suitable heliport. While the heliport itself may be simple, the planning and organization necessary to properly develop a heliport can present challenges. Ensure proper consideration of the physical, technical, safety, and public interest matters described in this document during the planning and establishment of a heliport.

## 1.5 Existing Heliports.

Whenever a change or alteration to an existing heliport requires the submission of FAA Form 7460-1, Notice of Proposed Construction or Alteration, or FAA Form 7480-1, Notice of Landing Area Proposal, consider taking necessary actions, as practical, to bring the heliport up to current design standards. Refer to paragraph 1.11.3 for additional information.

## 1.6 Location.

The optimum location for a heliport is near the desired origination and/or destination of the potential heliport users. Industrial, commercial, and medical operations in urban locations are demand generators for helicopter services, even though they often compete for the limited ground space available.

## 1.6.1 Factors to Consider.

Heliport sites adjacent to a river, lake, railroad, freeway, or highway offer potential for multi-functional land usage.

Locations that have the advantage of unobstructed airspace and which have properly enacted zoning can provide further protection from disruptive encroachment.

Requirements for scheduled “airline-type” passenger services may necessitate the development of an instrument procedure to permit “all-weather” service.

## 1.7 AC Organization.

This AC covers GENERAL AVIATION heliports (including PPR heliports), TRANSPORT heliports, HOSPITAL heliports, and emergency landing facilities. Heliport proponent familiarity with the terminology used in this specialized field is imperative. See paragraph 1.8 for specific heliport terminology and definitions.

## 1.7.1 Helicopter Facilities on Airports.

Consider developing separate heliport facilities for helicopter use when there are a significant number of helicopter operations on an airport. Chapter 5 addresses helicopter facilities on airports.

## 1.7.2 Instrument Operations.

Instrument approach procedures at heliports are practical since the introduction of the global positioning system (GPS). Good planning suggests that heliport proponents plan for the eventual development of instrument approaches to their heliports. Consider the recommendations in Chapter 6 in contemplating future instrument operations at a heliport during heliport site selection and design, even if the heliport will not initially have instrument operations.

## 1.7.3 Heliport Gradients and Pavement Design.

Chapter 2 provides guidance on heliport gradients and pavement design issues.

## 1.7.4 Additional Information and Resources.

Additional information and resources are found in the Appendices as follows:

• Appendix A provides guidance on emergency helicopter landing facilities.

• Appendix B provides guidance for pre-designated emergency landing areas.

Appendix C provides helicopter dimensional data.

Appendix D provides guidance on the form, size, and proportions of certain heliport markings.

Appendix E provides a list of associated publications and resources referenced in this AC.

• Appendix F provides a heliport evaluation process flow chart.

Appendix G provides design guidance on heliport lighting.

## 1.8 Explanation of Terms.

The Pilot/Controller Glossary of the Aeronautical Information Manual (AIM) defines terms used in the Air Traffic System. Copies of the AIM are available from the FAA website https://www.faa.gov/air\_traffic/publications/. Other terms used in this publication follow.

## 1.8.1 Air Taxi.

Refers to helicopter taxi operations, typically below 100 feet (30.5 m) above ground level (AGL), which allows helicopter movement from one point to another.

## 1.8.2 Approach/Departure Path.

## 1.8.3 Controlling Dimension (D).

The greater of helicopter overall length (OL) and overall width (OW).

## 1.8.4 Design Helicopter.

A single or composite helicopter that reflects the maximum weight, maximum contact load/minimum contact area, controlling dimension (D), overall width (OW), rotor diameter (RD), tail rotor arc radius, undercarriage dimensions, and pilot’s eye height of all helicopters expected to operate at the heliport.

## 1.8.5 Design Loads.

Design and construct the touchdown and lift area (TLOF), and any load-bearing surfaces, to support the loads imposed by the design helicopter and any ground support vehicles and equipment.

## 1.8.5.1 Static Load.

For design purposes, the design static load is equal to the helicopter’s maximum takeoff weight applied through the total contact area of the wheels or skids. See paragraph 2.7.3.1.

## 1.8.5.2 Dynamic Load.

For design purposes, assume the dynamic load at 150 percent of the maximum takeoff weight of the design helicopter applied through the main undercarriage on a wheel-equipped helicopter or aft contact areas of skidequipped helicopter. See paragraph 2.7.3.2.

## 1.8.6 Elevated Heliport.

A heliport located on a rooftop or other elevated structure where the TLOF is at least 30 inches (0.8 m) above the surrounding surface (a ground-level heliport with the TLOF on a mound is not an elevated heliport).

## 1.8.7 Emergency Helicopter Landing Facility (EHLF).

A clear area at ground level or on the roof of a building capable of accommodating helicopters engaged in fire fighting and/or emergency evacuation operations. An EHLF meets the definition of a heliport in this AC and under 14 CFR Part 157, Notice of Construction, Alteration, Activation, and Deactivation of Airports.

## 1.8.8 Final Approach and Takeoff Area (FATO).

A defined area over which the pilot completes the final phase of the approach to a hover or a landing and from which the pilot initiates takeoff. The FATO and TLOF are normally co-located but may be located separately. The FATO is associated with all instrument approach/departure procedures.

1.8.9 Final Approach Reference Area (FARA). An obstacle-free area with its center aligned on the final approach course. It is located at the end of a precision instrument FATO.

1.8.10 Frangibly Mounted. While there is no accepted standard for frangibility regarding helicopter operations, remove all objects from a FATO and safety area except those of the lowest mass practicable and frangibly mounted objects no higher than 2 inches (51 mm) above the adjacent TLOF elevation, to the extent practicable.

A heliport intended to accommodate individuals, corporations, aerial tourism, and public safety agencies. For the purposes of this AC, “general aviation” refers to all helicopter operations other than scheduled service (with the exception of unscheduled service with helicopters with maximum takeoff weight (MTOW) greater than 12,500 pounds (lbs)). HOSPITAL heliports and emergency landing facilities fall under general aviation but are treated separately in the AC due to their specific requirements. GENERAL AVIATION heliports may be publicly or privately owned.

1.8.12 Ground Taxi. The surface movement of a wheeled helicopter under its own power with wheels touching the ground.

1.8.13 Hazard to Air Navigation. An existing or proposed object that the FAA, as a result of an aeronautical study, determines will have a substantial adverse effect upon the safe and efficient use of navigable airspace by helicopters and other aircraft, operation of air navigation facilities, or existing or potential airport capacity.

1.8.14 Helipad. A small, designated area, usually with a prepared surface, on a heliport, airport, landing/takeoff area, apron/ramp, or movement area used for takeoff, landing, or parking of helicopters. A helipad on an airport does not constitute a heliport.

1.8.15 Heliport. An area of land, water, or structure used or intended to be used for helicopter landings and takeoffs and includes associated buildings and facilities.

1.8.16 Heliport Elevation. The highest elevation of all helicopter landing areas (TLOFs) within the heliport, expressed as the distance above mean sea level (MSL).

1.8.17 Heliport Imaginary Surfaces. The imaginary planes defined in 14 CFR Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, centered about the FATO and the approach/departure paths, which are used to identify the objects where notice to and evaluation by the FAA is

required. Recommendations for mitigating possible obstructions to air navigation may include realignment of approach/departure paths or removal, lowering, marking, and lighting of objects.

## 1.8.18 Heliport Layout Plan.

The plan of a heliport showing the layout of existing and proposed heliport facilities including the approach/departure paths and dimensions of TLOF, FATO, and Safety Area.

## 1.8.19 Heliport Protection Zone (HPZ).

An area off the end of the FATO and under the approach/departure path intended to enhance the protection of people and property on the ground.

## 1.8.20 Heliport Reference Point (HRP).

The geographic position of the heliport expressed as the latitude and longitude at:

The center of the FATO, or the centroid of multiple FATOs, for heliports having visual and non-precision instrument approach procedures; or

The center of the final approach reference area (FARA) when the heliport has a precision instrument procedure.

## 1.8.21 Helistop.

A heliport that provides no fueling, defueling, maintenance, repairs, or storage of helicopters. The geometry and approach/departure surfaces of a helistop are identical to those of a heliport. This AC does not use this term, as the design standards and recommendations in this AC apply to all heliports.

## 1.8.22 HOSPITAL Heliport.

A HOSPITAL heliport services helicopters used by helicopter air ambulance providers. A HOSPITAL heliport may be designed to accommodate large military helicopters in some emergencies. Air ambulance helicopters are often used to transport injured persons from the scene of an accident to a hospital and to transfer patients from one hospital to another. A designated helicopter landing area located at a hospital or medical facility is a heliport and not a medical emergency site.

## 1.8.23 Hover Taxi.

The movement of a helicopter above the surface, typically used to move short distances from one point to another. Generally, this takes place at a wheel/skid height of 1 to 5 feet (0.3 to 1.5 m) and at a slow ground speed of less than 20 knots (37 kilometers(km)/h). For facility design purposes, assume a skid-equipped helicopter to hover-taxi.

## 1.8.24 In-Pavement Lights.

Where the term “in-pavement lights” is specified in this AC, interpret it as including inground lights.

1.8.25 Landing Position. An area, normally located in the center of an elongated TLOF, on which the helicopter lands.

1.8.26 Large Helicopter. A helicopter with a maximum takeoff weight of more than 12,500 lbs (5,670 kilograms (kg)).

1.8.27 Load-Bearing Area (LBA). The portion of the TLOF and any additional support structure capable of supporting the dynamic load of the design helicopter.

1.8.28 Medical Emergency Site. An unprepared site at or near the scene of an accident or similar medical emergency on which a helicopter may land to pick up a patient to provide emergency medical transport. A medical emergency site is not a heliport as defined in this AC.

1.8.29 Medium Helicopter. A helicopter with a maximum takeoff weight of more than 7,000 lbs (3,175 kg) and up to 12,500 lbs (5,670 kg).

1.8.30 Obstruction to Air Navigation. Any fixed or mobile object, including a parked helicopter, of greater height than any of the heights or surfaces presented in subpart C of Part 77.

1.8.31 Overall Helicopter Length (OL). The overall length of the helicopter, which is the dimension from the tip of the main or forward rotor to the tip of the tail rotor, fin, or other rear-most point of the helicopter. This value is with the rotors at their maximum extension. See Appendix C. If only the value of the RD is known, estimate the value for OL using the relationship OL = 1.2 RD (or conversely, RD = 0.83 OL).

1.8.32 Overall Width (OW). The OW is defined as the maximum outer dimension of the aircraft rotors or wings. See Appendix C.

1.8.33 Parking Pad. The center portion of a helicopter parking position, whether paved or grass.

A heliport developed for exclusive use of the owner and persons authorized by the owner and about which the owner and operator ensure all authorized pilots are thoroughly knowledgeable. These features include but are not limited to:

approach/departure path characteristics

• preferred heading

obstacles in the area

size and weight capacity of the facility

• heliport facility limitations

1.8.35 Public-use Heliport. A heliport available for use by the public without a requirement for prior approval of the owner or operator.

1.8.36 Rotor Diameter (RD). The length of the main rotor, from tip to tip.

1.8.37 Rotor Downwash. The downward movement of air caused by the action of the rotating main rotor blades. When this air strikes the ground or some other surface, it causes a turbulent outflow of air from beneath the helicopter.

1.8.38 Safety Area. A defined area on a heliport surrounding the FATO intended to reduce the risk of damage to helicopters accidentally diverging from the FATO.

1.8.39 Shielded Obstruction. A proposed or existing obstruction that does not need to be marked or lighted due to its proximity to another obstruction whose highest point is at the same or higher elevation.

1.8.40 Shoulder Line. A marking line perpendicular to a helicopter parking position centerline that is intended to provide the pilot with a visual cue to assist in parking.

1.8.41 Small Helicopter. A helicopter with a maximum takeoff weight of 7,000 lbs (3,175 kg) or less.

1.8.42 Tail Rotor Arc Radius. The distance from the hub of the main rotor to the outermost tip of the tail rotor or the rear-most point of the helicopter tail, whichever is farther.

1.8.43 Takeoff Position. An area, normally located on the centerline and at the ends of an elongated TLOF, from which the helicopter takes off. Typically, there are two such positions on an elongated TLOF, one at each end.

1.8.44 Taxi Route. An obstruction-free corridor established for the movement of helicopters from one part of a heliport/airport to another. A taxi route includes the taxiway plus the appropriate clearances on both sides.

## 1.8.45 Taxiway.

A marked route between the TLOF and other areas on the heliport. This AC defines two types of helicopter taxiways:

1.8.45.1 Ground Taxiway. A taxiway intended to permit the surface movement of a wheeled helicopter under its own power with wheels on the ground. The minimum dimensions defined for a ground taxiway may not be adequate for hover taxi.

1.8.45.2 Hover Taxiway. A taxiway intended to permit the hover taxiing of a helicopter.

1.8.46 Touchdown and Liftoff Area (TLOF). A load-bearing (generally paved) area normally centered in the FATO, on which the helicopter performs a touchdown or liftoff.

1.8.47 Transitional Surface. An imaginary surface which, in conjunction with the approach/departure surface, provides airspace clear of hazards to allow safe approaches to, and departures from, the FATO.

## 1.8.48 TRANSPORT Heliport.

A heliport designed to accommodate air carriers providing scheduled service on large helicopters (helicopters with a maximum takeoff weight greater than 12,500 lbs (5,670 kg)). Extensive airside and landside infrastructure is provided to accommodate passengers and to enable operations in instrument meteorological conditions.

## 1.8.49 Touchdown/Positioning Circle (TDPC) Marking.

A circular marking located in the center of a TLOF or a parking position. When the pilot’s seat is over the TDPC, the whole of the helicopter undercarriage will be within the TLOF or parking position, and all parts of the helicopter rotor system, will be clear of any obstacle by a safe margin.

1.8.50 Undercarriage Width (UCW). The distance between the outside edges of the outer tires or skids. See Figure B-1.

1.8.51 Unshielded Obstruction. A proposed or existing obstruction that may need to be marked or lighted since it is not near another marked and lighted obstruction whose highest point is at the same or higher elevation.

## 1.9 Selection of Approach/Departure Paths.

Design heliports to the extent practicable for two approach/departure paths. Consider wind, obstructions, and environmental impacts, for example, in selecting the approach/departure paths.

## 1.9.1 Wind.

Well-designed approach/departure paths permit pilots to avoid downwind conditions and minimize crosswind operations. Align the preferred flight approach paths and departure paths, to the extent feasible, with the predominant wind direction. Base other approach paths and departure paths on the assessment of the prevailing winds or, when this information is not available, separate such flight paths and the preferred flight path by at least 135 degrees. If it is not feasible to provide adequate coverage of wind conditions through multiple approach/departure paths, operational limitations may be necessary under certain wind conditions. See paragraph 2.12.1.

## 1.9.2 Obstructions.

In determining approach/departure paths, consider any existing or proposed (future) obstructions near the heliport and those likely to be a hazard to air navigation. See paragraph 1.11.

## 1.9.3 Environmental Impacts.

In environmentally sensitive areas, select the final approach/departure path(s) to minimize any environmental impact, providing it does not decrease flight safety. See paragraph 1.13.

## 1.10 Notification Requirements.

Part 157 sets requirements for persons proposing to construct, activate, deactivate, or alter a heliport to give advance notice of their intent to the FAA. This includes but is not limited to the following changes:

• changing the size or number of FATOs;

• adding, deleting, or changing an approach or departure route;

change to a heliport status (for example, changing the heliport status) from private to public-use or vice versa.

File FAA Form 7480-1 (see Figure 1-1) with the appropriate FAA Airports Regional or District Office at least 90 days before construction, alteration, deactivation, or change in use when notification is required. See the FAA Airports website at https://www.faa.gov/airports/ for contact information. Alterations to an existing heliport requiring notification could include changes to heliport dimensions, approach and departure surfaces, heliport location, and heliport relocation to a different site.

Appendix F provides the general heliport evaluation process flow chart to be followed by heliport proponents.

## 1.10.1 Draw the heliport layout plan to scale showing key dimensions, such as:

heliport elevation

TLOF size

FATO size

safety area size

distance from safety area perimeter to property edges

approach/departure paths showing locations of:

o buildings

o trees

fences

o power lines

o obstructions (including elevations)

o schools

o churches

o hospitals

o residential communities

o waste disposal sites

o other significant features, as specified on FAA Form 7480-1 and shown in Figure 1-2.

1.10.2 The preferred type of heliport location map using current web-based satellite imagery. Show the location of the heliport site and the approach/departure paths on the map. Point out the heliport site on this map with a red arrow. Indicate the latitude and longitude of the proposed heliport in North American Datum of 1983 (NAD-83) coordinates. See Figure 1-3.

Figure 1-1. FAA Form 7480-1, Notice for Construction, Alteration and Deactivation of Airports
<table><tr><td rowspan=1 colspan=13>U.S. Depatment of Transportation                                                      OMBCONTROLNUMBER:2120-0036Federal Aviation Administration                                                          EXPIRATIONDATE:11/30/2022</td></tr><tr><td rowspan=1 colspan=13>NOTICE FOR CONSTRUCTION, ALTERATION AND DEACTIVATION OF AIRPORTS</td></tr><tr><td rowspan=1 colspan=6>A. Airport Owner       Check if this is also the Property Owner</td><td rowspan=1 colspan=7>B. Airport Manager (Complete if different than the Airport Owner)</td></tr><tr><td rowspan=1 colspan=6>1.Name and Address    Check if this is the Airport&#x27;s Physical Address</td><td rowspan=1 colspan=7>1.Name and Address      Check if this is the Airport&#x27;s Physical Address</td></tr><tr><td rowspan=1 colspan=3>2.Phone</td><td rowspan=1 colspan=3>3.Email</td><td rowspan=1 colspan=4>2.Phone</td><td rowspan=1 colspan=3>3.Email</td></tr><tr><td rowspan=1 colspan=6>C. Purpose of Notification (Answer allquestions that apply)</td><td rowspan=1 colspan=7>D. Name, Location, Use and Type of Landing Area</td></tr><tr><td rowspan=1 colspan=1>1.Construct orEstablish an:</td><td rowspan=1 colspan=5>AiportUtralight Fightpark□BallonportHeliport□Seaplane Base   □Other</td><td rowspan=1 colspan=6>1.Name of Landing Area</td><td rowspan=1 colspan=1>2.Loc ID (for existing)</td></tr><tr><td rowspan=1 colspan=1>2.Construct, AlterorRealign a</td><td rowspan=1 colspan=5>□Runway□Helipad(s)      □other□TaxiwayPublic UseAiports only)</td><td rowspan=1 colspan=6>3.Associated City and State</td><td rowspan=1 colspan=1>4.Distance from City(mm)</td></tr><tr><td rowspan=1 colspan=1>3.Change StatusFrom/To:</td><td rowspan=1 colspan=5>□VFR to IFR         □IFR to VFR□Private Use to Public Use□Public Use to Other</td><td rowspan=1 colspan=6>5.County(Physical Location)</td><td rowspan=1 colspan=1>6.Direction from City</td></tr><tr><td rowspan=2 colspan=1>4.Change Traff cPattern</td><td rowspan=2 colspan=5>□DIRECTION:ALTITUDEChee Litalitueif nortannTurbo:std.nonstd.   Prop:□stdnonstd.Helo. std nonstd.    Otter Describein boxC6.</td><td rowspan=1 colspan=4>7.Latitude。  1       =</td><td rowspan=1 colspan=2>8. Longitude。   1       &quot;</td><td rowspan=1 colspan=1>9.Elevation</td></tr><tr><td rowspan=1 colspan=2>10.CurentUse:</td><td rowspan=1 colspan=5>PrivatePublic Private Use of Public Lands</td></tr><tr><td rowspan=1 colspan=1>5.Deactivate</td><td rowspan=1 colspan=5>Airpot RWY       □TWY</td><td rowspan=1 colspan=2>11.Ownership</td><td rowspan=1 colspan=5>□PrivatePublic Military(Branch)</td></tr><tr><td rowspan=1 colspan=6>6. Description:</td><td rowspan=1 colspan=7>12.Airport    □Airport Ultralight Flihtpark BallonportHeliport(applicable elecAmbulanceLaw EnforcementType:      Fire Protection) Seaplane Base□Other</td></tr><tr><td rowspan=1 colspan=6>E. Landing Area Data (List any Proposed, New or Unregistered Runways, Helipads etc.)</td><td></td><td></td><td></td><td></td><td></td><td></td><td></td></tr><tr><td rowspan=1 colspan=6>1.Airport, Seaplane Base or Ultralight Flightpark (use second pageif needed)</td><td rowspan=1 colspan=7>2.Heliport, Balloonport or other Landing Area (use second pageif needed)</td></tr><tr><td rowspan=1 colspan=2>RWY ID</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=3>Helipad ID</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Lat. &amp; Long.</td><td rowspan=1 colspan=2>Show on attachment(s)</td><td rowspan=1 colspan=2>Showon attachment(s)</td><td rowspan=1 colspan=3>Lat. &amp; Long.</td><td rowspan=1 colspan=3>Show on atachment(s)</td><td rowspan=1 colspan=1>Show on attachment(s)</td></tr><tr><td rowspan=1 colspan=2>Surface Type</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>Surface Type</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Length feet)</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>TLOF Dimensions</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Width feet)</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>FATO Dimensions</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Lighting (f any)</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>Lighting (if any)</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Right Tratic (YN)</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=3>Ingress/Egress (Degrees)</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>Elevation (AMSL)</td><td rowspan=1 colspan=2>Show on attachment(s)</td><td rowspan=1 colspan=2>Showon attachment(s)</td><td rowspan=1 colspan=3>Elevation (AMSL)</td><td rowspan=1 colspan=3>Showon attachment(s)</td><td rowspan=1 colspan=1>Show on attachment(s)</td></tr><tr><td rowspan=1 colspan=2>VFR or IFR</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=2>/</td><td rowspan=1 colspan=3>Elevated Height (AGL)</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=2>F.Operational Dat</td><td rowspan=1 colspan=11>F. Operational Data (Indicate if the number provided is Actual or Estimated)</td></tr><tr><td rowspan=2 colspan=2></td><td rowspan=1 colspan=5>1.Number of Based Aircraft</td><td rowspan=1 colspan=6>2.Average Number of Monthly Landings</td></tr><tr><td rowspan=1 colspan=3>Present or Estim ated</td><td rowspan=1 colspan=2>Estimated in 5 Years</td><td rowspan=1 colspan=4>Present or Estimated</td><td rowspan=1 colspan=2>Estimated in 5 Years</td></tr><tr><td rowspan=1 colspan=2>Single Engine</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Muli Engine</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Jet</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Helicopter</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Glider</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Military</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=2>Utralight</td><td rowspan=1 colspan=3></td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=4></td><td rowspan=1 colspan=2></td></tr><tr><td rowspan=1 colspan=13>3haie</td></tr><tr><td rowspan=1 colspan=13>4.Are IFRProcedures forthe Airport Anticipated?□Yes□No.IfYes,within    _years</td></tr><tr><td rowspan=1 colspan=13>G.CERTereycerify hatalof theabvestateertsae earetreancopleteheestofy wee.</td></tr><tr><td rowspan=2 colspan=5>1.Name,tite of person fing this notice (ype or prit)</td><td rowspan=1 colspan=8>2.Signature (inink)</td></tr><tr><td rowspan=1 colspan=8>3.Date           4.Phone           5.Email</td></tr></table>

FAAForm7480-1(7/20)SUPERSEDES PREVIOUSEDITION

See online FAA Form 7480-1.

Figure 1-2. Example of a Heliport Layout Plan  
![aab44105c3661a2be5cdefdc78c6cda03d393644d2486f5b000b17d541cfe4fe.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/aab44105c3661a2be5cdefdc78c6cda03d393644d2486f5b000b17d541cfe4fe.jpg)  
Draw heliport layout plan to scale with key dimensions and locations, including:  
a. TLOF and FATO size  
b. Safety area dimensions  
c. Distances from the safety area perimeter to property boundaries, buildings, etc.  
d. Site furnishings (bollards, signs, benches, and other site accessories)  
See Chapter 2 for guidance on heliport facility sizes and shapes.

Figure 1-3. Example of a Heliport Location Map  
![ff189cb2583d62893e625378de1c8c557a241e6e0e28606676ad17fe99c79615.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ff189cb2583d62893e625378de1c8c557a241e6e0e28606676ad17fe99c79615.jpg)

## 1.10.3 The FAA Role.

The FAA will conduct an aeronautical study of the proposed heliport under § 157.7, FAA Determinations. Part (a) of this section of the regulation states:

“The FAA will conduct an aeronautical study of an airport proposal and, after consultations with interested persons, as appropriate, issue a determination to the proponent and advise those concerned of the FAA determination. The FAA will consider matters such as the effects the proposed action would have on existing or contemplated traffic patterns of neighboring airports; the effects the proposed action would have on the existing airspace structure and projected programs of the FAA; and the effects that existing or proposed manmade objects (on file with the FAA) and natural objects within the affected area would have on the airport proposal. While determinations consider the effects of the proposed action on the safe and efficient use of airspace by aircraft and the safety of persons and property on the ground, the determinations are only advisory. Except for an objectionable determination, each determination will contain a determinationvoid date to facilitate efficient planning of the use of the navigable airspace. A determination does not relieve the proponent of responsibility for compliance with any local law, ordinance or regulation, or state or other federal regulation. Aeronautical studies and determinations will not consider environmental or land use compatibility impacts.”

## 1.10.4 Penalty for Failure to Provide Notice.

Persons who fail to give notice are subject to civil penalty under Title 49 United States Code 46301, Civil Penalties, of not more than \$25,000 (or \$1,100 if the person is an individual or small business concern).

## 1.10.5 Notice Exemptions.

Section 157.1, Applicability, exempts sites meeting one of the conditions below from the requirement to submit notice. These exemptions do not negate a notice or formal approval requirement prescribed by state law or local ordinance. For the purposes of applying the Part 157 exemption criteria cited in (2) and (3) below, a landing and associated takeoff is considered one operation. Section 157.1 projects are:

[A heliport] subject to conditions of a federal agreement that requires an approved current heliport layout plan to be on file with the FAA, or

[A heliport] at which flight operations will be conducted under visual flight rules (VFR) and which is used or intended to be used for a period of less than 30 consecutive days with no more than ten operations per day.

The intermittent use of a site that is not an established airport, that is used or intended to be used for less than one year, and at which flight operations will be conducted only under VFR. For this part, “intermittent use of a site” means:

a. the site is used or is intended to be used for no more than three days in any one week, and

b. no more than ten operations will be conducted in any one day at that site.

## 1.11 Hazards to Air Navigation.

Part 77 establishes requirements for notification to the FAA of objects that may affect navigable airspace. See Figure 1-4 for examples of development requiring notice to the FAA.

Part 77 sets standards for determining obstructions to navigable airspace and provides for aeronautical studies of such obstructions to determine their effect on the safe and efficient use of airspace. Part 77 applies only to the following:

public heliports and public airports;

airports operated by a federal agency or the Department of Defense (DoD); and

private airports and heliports with at least one FAA-approved instrument approach procedure.

## 1.11.1 FAA Studies.

## 1.11.1.1 Part 77.

Part 77 defines objects that are obstructions to surfaces. Presume these objects to be hazards to air navigation unless an FAA study determines otherwise. The FAA conducts aeronautical studies to determine the

physical and electromagnetic effect on the use of navigable airspace, air navigational facilities, public airports and heliports, and private airports and heliports with at least one FAA-approved instrument approach procedure. The FAA encourages public agencies to enact zoning ordinances to prevent man-made features from becoming hazards to navigation.

## 1.11.1.2 Part 157.

FAA aeronautical studies performed under Part 157 establish standards and notification requirements for anyone proposing to construct, alter, or deactivate a civil or joint-use (civil/military) airport or heliport. This regulation also addresses proposals that alter the status or use of airport or heliport facilities.

## 1.11.2 Mitigation of Hazards.

You may mitigate the adverse effect of an object presumed or determined to be a hazard by:

Removing the object.

Altering the object, for example, reducing its height.

Marking and/or lighting the object, provided an FAA aeronautical study has determined that the object would not be a hazard to air navigation if it were marked and/or lighted. Find guidance on marking and lighting objects in AC 70/7460-1, Obstruction Marking and Lighting.

## 1.11.3 Notification Requirements.

Part 77 requires persons proposing certain construction or alteration to give a 45-day notice to the FAA of their intent. Use FAA Form 7460-1, Notice of Proposed Construction or Alteration, to provide notification. See https://oeaaa.faa.gov/ for more information and to download FAA Form 7460-1. Alterations to an existing heliport requiring notification could include changes to heliport dimensions, approach and departure surfaces, heliport location, and heliport relocation to a different site.

Figure 1-4. Offsite Development Requiring Notice to the FAA  
![ac428eee1affe067e8de92c6ea2d69c7e5a4bfd3b4984afe433345bf110ae3cb.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ac428eee1affe067e8de92c6ea2d69c7e5a4bfd3b4984afe433345bf110ae3cb.jpg)  
Notice under Part 77 is required for all public-use heliports or private-use heliports with at least one FAA-approved instrument approach procedure.

## Offsite Development Examples for Figure 1-4:

① Building is less than 200 feet (ft) (61 meters (m)) in height, but top will penetrate the 25:1 surface (notice required by § 77.9).

② Antenna is over 200 ft (61 m) in height (notice is required by § 77.9(a)).

③ Antenna is less than 200 ft (61 m) in height and penetrates the 25:1 surface (notice is required by § 77.9(b)(3)).

④ Construction crane penetrates 25:1 surface (notice is required by § 77.9(b)(3)).

⑤ Building is less than 200 ft (61 m) in height and does not penetrate the 25:1 surface (notice is not required).

⑥ Building is more than 5,000 ft (1,524 m) from heliport (notice is required if building will be 200 ft (61 m) or more in height).

## 1.11.4 Heliport Development Plans.

Future public heliport development plans and feasibility studies on file with the FAA may influence the determinations resulting from Part 77 studies. Owners of public and private heliports with FAA-approved instrument approach procedures can ensure full consideration of future heliport development in Part 77 studies only when they file plans with the FAA. Ensure the coordinates and elevations of planned FATO(s),

approach/departure paths including their azimuths, and types of approaches for any new FATO or modification of an existing FATO are included in heliport plan data.

## 1.12 Federal Assistance.

The FAA administers a grant program that provides financial assistance to eligible sponsors to develop a public-use heliport. Information on federal aid program eligibility requirements is available from FAA Airports Regional and District Offices and on the FAA Airports website, www.faa.gov/airports.

## 1.13 Environmental Impact Analyses.

The National Environmental Policy Act (NEPA) of 1969 requires the FAA to consider potential environmental impacts prior to agency decision making, including, for example, the decision to fund or approve a project, plan, license, permit, certification, rulemaking, or operations specification. Actions that may warrant an environmental review are normally associated with federal grants or airport layout plan (ALP) approvals leading to the construction of a new heliport or significant expansion of an existing heliport.

## 1.13.1 Environmental Review Items.

An environmental review addresses noise, historic and cultural resources, wildlife, energy conservation, land usage, air quality, water quality, pollution prevention, light emissions, and other visual effects, and other public health and safety issues. The review evaluates the “no action” alternative and a reasonable range of feasible alternatives, including mitigation not included in the initial alternative. The review will also describe actions taken to ensure public involvement in the planning process. An opportunity for a public hearing may be required for the federally funded development of, or significant improvement to, an existing heliport.

## 1.13.2 Guidance.

FAA Order 1050.1, Polices and Procedures for Considering Environmental Impacts, FAA Order 5050.4, National Environmental Policy Act (NEPA) Implementing Instructions for Airport Projects, and other supplemental guidance from FAA Air Traffic and Flight Standards provide guidance on environmental impact analysis. Contact state and local governments, including metropolitan planning organizations and local transit agencies, directly, as they may also necessitate an environmental report. The procedures in AC 150/5020-1, Noise Control and Compatibility Planning for Airports, describe a means of assessing the noise impact. Contact the appropriate FAA Airports Regional or District Office for current information related to assessing the noise impact of heliports. Proponents of non-federally assisted heliports work with local governmental authorities concerning environmental issues.

## 1.14 Terminal Facilities Design Considerations.

A heliport terminal provides curbside access for passengers using private autos, taxicabs, and public transit vehicles. Public waiting areas need the usual amenities, and a counter for rental car services may be desirable. Design passenger auto parking areas to accommodate current requirements, with the ability to expand them to meet future requirements. Readily available public transportation may reduce the requirement for employee and service personnel auto parking spaces. Build attractive and functional heliport terminal buildings or sheltered waiting areas. Guidance on designing terminal facilities is provided in AC 150/5360-13, Airport Terminal Planning.

At PPR heliports, the number of people using the facility may be so small that there is no need for a terminal building, and minimal needs for other facilities and amenities.

## 1.14.1 Security – TRANSPORT Heliports.

Unless screening was carried out at the helicopter passengers’ departure location, Transportation Security Administration regulations may require that a screening area and/or screening be provided before passengers enter the airport’s secured areas. If needed, provide multiple helicopter parking positions and/or locations in the terminal area to service helicopter passenger and/or cargo interconnecting needs. Find information about passenger screening at the Transportation Security Administration website (https://www.tsa.gov/public/).

## 1.15 Zoning for Compatible Land Use.

The FAA encourages all heliport operators to promote the adoption of the following zoning measures where state and local statutes permit to ensure the heliport will continue to be available and to protect the investment in the facility.

## 1.15.1 Zoning to Limit Building/Object Heights.

Find general guidance on drafting an ordinance that would limit building and object heights in AC 150/5190-4, A Model Zoning Ordinance to Limit Height of Objects Around Airports. Substitute the heliport surfaces for the airport surfaces described in the model ordinance.

## 1.15.2 Zoning for Compatible Land Use.

The FAA encourages public agencies to enact zoning ordinances to control the use of property within the HPZ and the approach/departure path environment, restricting activities to those that are compatible with helicopter operations. See paragraph 2.13.

## 1.15.3 Air Rights and Property Easements.

Use air rights and property easements as options to prevent the encroachment of obstacles near a heliport.

## 1.16 Access to Heliports by Individuals with Disabilities.

Congress has passed various laws concerning access to airports. Since heliports are a type of airport, these laws are similarly applicable. Find guidance in AC 150/5360-14, Access to Airports by Individuals with Disabilities.

## 1.17 State Role.

Many state departments of transportation, aeronautical commissions, or similar authorities require prior approval and, in some instances, a license for the establishment and operation of a heliport. Several states administer a financial assistance program like the federal program and are staffed to provide technical advice. Contact your respective state aeronautics commissions or departments for specifics on licensing and assistance programs. Contact information for state aviation agencies is available at https://www.faa.gov/airports/resources/state\_aviation.

## 1.18 Local Role and Building Code.

Some communities have enacted zoning laws, building codes, fire regulations, etc., that can affect heliport establishment and operation. Most municipalities have a formal process such as a “Conditional Use Permit” in place for the establishment of a heliport. Check with your local Planning and Zoning Commission for details. Some have or are in the process of developing codes or ordinances regulating environmental issues such as noise and air pollution. A few localities have enacted specific rules governing the establishment of a heliport. Therefore, make early contact with officials or agencies representing the local zoning board, the fire, police, or sheriff's department, and elected personnel who represent the area where the heliport is to be located.

## 1.19 Related Referenced Material.

Find a list of associated publications and references in Appendix E.

# CHAPTER 2. Heliport Design

## 2.1 General.

This chapter provides guidance on the design of heliports. There are three types of heliports. GENERAL AVIATION, TRANSPORT, and HOSPITAL. Figure 2-1, Figure 2-2, and Figure 2-3 show basic features of these three heliport types. See paragraph 1.8 for descriptions of the three heliport types. This chapter provides general heliport design guidance and also highlights any differences in design elements among the types of heliports.

## 2.2 Prior Permission Required (PPR) Facilities.

Unless required by federal law or regulation, the recommendations in this AC are not mandatory for PPR heliports. Recommendations for PPR heliports are provided due to the specific nature of these heliport facilities where the operator ensures that pilots are thoroughly familiar with the heliport, its procedures, and any facility limitations.

## 2.3 Design Approach.

The design standards in this chapter assume that there will never be more than one helicopter within the FATO and the associated safety area. A TLOF can be located within the FATO or outside the FATO, as described in paragraph 2.7.

## 2.4 Access by Individuals with Disabilities.

Various laws require heliports operated by public entities and those receiving federal financial assistance to meet accessibility requirements. See paragraph 1.16.

Figure 2-1. GENERAL AVIATION Heliport – Basic Features  
![c9254dad93e672a5adbdea2a1888b4a83255d98cc24e575b6151ad8c46c8a886.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c9254dad93e672a5adbdea2a1888b4a83255d98cc24e575b6151ad8c46c8a886.jpg)  
See Chapter 4 for guidance on heliport markings.  
Locate the wind cone outside of the Safety Area. Ensure the wind cone and any security fencing or security barrier will not interfere with the approach/departure surface or transitional surface.

Figure 2-2. TRANSPORT Heliport – Basic Features  
![d795de1fbb3cbeefaccd2538356f543e6dcae4c2993f369ccfc7b94562f74145.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d795de1fbb3cbeefaccd2538356f543e6dcae4c2993f369ccfc7b94562f74145.jpg)  
See Chapter 4 for guidance on heliport markings.  
Locate the wind cone outside of the Safety Area. Ensure that the wind cone and any security fencing or security barrier will not interfere with the approach/departure surface or transitional surface.

Figure 2-3. HOSPITAL Heliport (Ground Level) – Basic Features  
![58fca2a4a0c7d1b78b3842e8702053726d2e30d06cb9b58d5162f70957525bd1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/58fca2a4a0c7d1b78b3842e8702053726d2e30d06cb9b58d5162f70957525bd1.jpg)  
Locate the security fence and wind cone outside of the Safety Area. Ensure that the wind cone and any security fencing or security barrier will not interfere with the approach/departure surface or transitional surface.

See Chapter 4 for guidance on heliport markings.

## 2.5 Heliport Site Selection.

## 2.5.1 Long-term Planning.

The FAA encourages public agencies and others planning to develop a GENERAL AVIATION, TRANSPORT, or HOSPITAL heliport to consider the possible future need for instrument operations and facility expansion. Consider any current or future potential use by military helicopters that may be used in disaster relief efforts during planning for HOSPITAL heliports.

## 2.5.2 Property Requirements.

The property needed for GENERAL AVIATION and TRANSPORT heliports is dependent upon the volume and types of users, helicopter sizes, and the scope of amenities provided for each type of heliport facility. Property requirements for helicopter operators and for passenger amenities frequently exceed the property needed for “airside” purposes. The area needed for heliport or helipad operations may be as simple as a cleared area on the ground, a wind cone, and a clear approach/departure path for day heliport operations.

## 2.5.3 Turbulence.

Air flowing around and over buildings, stands of trees, terrain irregularities, etc., can create turbulence on ground-level and roof-top heliports that may affect helicopter operations. Assess the turbulence and airflow characteristics near, and across the surface of the FATO, and along the final section of the approach/departure path to determine if an air gap among the roof, roof parapet or supporting structure, and/or some other turbulence mitigating design measure is necessary. Perform this assessment where the FATO is located near the edge and top of a building or structure, or within the influence of turbulent wakes from other buildings or structures. The FAA’s Technical Report FAA/RD-84/25, Evaluating Wind Flow around Buildings on Heliport Placement, addresses the wind’s effect on helicopter operations. Take the following actions in selecting a site to minimize the effects of turbulence, as described in paragraphs below.

## 2.5.3.1 Ground-Level Heliports.

Proximity of buildings, trees, and other large objects to ground-level heliports can cause air turbulence and affect helicopter operations. Locate the landing and takeoff area away from such objects to minimize air turbulence near the FATO and the approach/departure paths.

## 2.5.3.2 Elevated Heliports.

Establishing a 6-foot (1.8 m) or more air gap on all sides above the roof level will generally minimize the turbulent effect of air flowing over the roof edge. If an air gap is included in the elevated heliport design, keep it free of objects that would obstruct the airflow. Where it is impractical to include an air gap or other turbulence mitigating design measures, operational limitations may be necessary under certain wind conditions.

## 2.5.4 Electromagnetic Effects.

Nearby electromagnetic devices, such as a large ventilator motor, elevator motor, magnetic resonance imaging machine (MRI), or other devices that consume large amounts of electricity may cause temporary abnormalities in the helicopter magnetic compass and interfere with other onboard navigational equipment. Buried rebar or other objects made of iron/steel below the heliport surface have also been shown to interfere with a helicopter’s navigation instruments.

Be alert to the location of any such devices with respect to a HOSPITAL heliport. A warning sign alerting pilots to the presence of an MRI is recommended. Take steps to inform pilots of the MRI locations or other electromagnetic equipment that consume large amounts of electricity. Heliports are recommended to include Heliport electromagnetic interference (EMI) hazard marking and signage to alert pilots to potential EMI impacts, as shown in Figure 2-4 and Figure 2-5. Locate the EMI hazard sign at ingress/egress points on the heliport for maximum visibility.

For additional information, see the FAA’s Technical Report FAA/RD-92/15, Potential Hazards of Magnetic Resonance Imagers to Emergency Medical Service Helicopter Services.

Figure 2-4. Heliport EMI Hazard Marking  
![66f8ebb97d9d02cafb84dd77f55fa948fe131ccd0b79264e5dd9ac6dfb5f3b1a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/66f8ebb97d9d02cafb84dd77f55fa948fe131ccd0b79264e5dd9ac6dfb5f3b1a.jpg)  
Align the compass with magnetic north. Use arrows, as shown, to indicate the four cardinal headings (N, S, E, W) and four intercardinal headings (NE, SE, SW, and NW).  
Use a minimum dimension of a 6-foot (1.8 m) outer diameter and a 4-foot (1.2 m) inner diameter for the compass circle.  
Use blue paint for the compass circle and white paint for the inner portion of the compass. If necessary for visual contrast, use a one-foot white outline along the outer edge of the compass and arrows.

Figure 2-5. Heliport EMI Hazard Sign

# CAUTION

![f5452edd63d253b9de02bfc1d4bb461319e6a31b0ea79539ca0703c50d62036d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f5452edd63d253b9de02bfc1d4bb461319e6a31b0ea79539ca0703c50d62036d.jpg)

Strong Magnetic Field

Aircraft navigational instruments may be affected. Confirm accuracy of navigation instruments during all operations.

## 2.6 TLOF/FATO and Safety Area Relationships.

The relationship, minimum dimensions, and separation distances of the TLOF, FATO and safety area are shown in Figure 2-6 and Table 2-1. A heliport consists of the following:

A TLOF is typically located within a FATO but can be located outside of the FATO. See paragraph 2.7.1.

A safety area which surrounds the FATO.

Approach/departure surfaces to allow safe approaches to and departures from a heliport landing sites.

Figure 2-6. TLOF/FATO/Safety Area Relationships and Minimum Dimensions  
![f9d1b1f6113b58d6e0ebc5c4240022d8ea9821884ee0a80999dbfce4c9666243.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f9d1b1f6113b58d6e0ebc5c4240022d8ea9821884ee0a80999dbfce4c9666243.jpg)  
For a circular TLOF and FATO, dimensions A, B, C, and E refer to diameters.  
For a square TLOF and FATO, all sides of the TLOF and FATO have equal length (e.g., dimension E = dimension C and dimension A = dimension B).  
For a square TLOF with a rectangular FATO, dimension E ≠ dimension C.

Table 2-1. TLOF/FATO Minimum Dimensions 1
<table><tr><td rowspan=1 colspan=1>Dim</td><td rowspan=1 colspan=1>Item</td><td rowspan=1 colspan=1>GA</td><td rowspan=1 colspan=1>TRANSPORT</td><td rowspan=1 colspan=1>HOSPITAL</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>TLOF Width</td><td rowspan=1 colspan=1>0.83D</td><td rowspan=1 colspan=1>0.83 D but not less than50 ft (15.2 m)</td><td rowspan=1 colspan=1>0.83 D but not lessthan 40 ft (12.2 m)</td></tr><tr><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>TLOF Length</td><td rowspan=1 colspan=1>0.83D</td><td rowspan=1 colspan=1>0.83 D but not less than50 ft (15.2 m)</td><td rowspan=1 colspan=1>0.83 D but not lessthan 40 ft (12.2 m)</td></tr><tr><td rowspan=1 colspan=1>C</td><td rowspan=1 colspan=1>FATO Length 2</td><td rowspan=1 colspan=1>1.50D</td><td rowspan=1 colspan=1>1.66 D but not less than100 ft (30.5 m)</td><td rowspan=1 colspan=1>1.50D</td></tr><tr><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>FATO Width</td><td rowspan=1 colspan=1>1.50D</td><td rowspan=1 colspan=1>1.66 D but not less than100 ft (30.5 m)</td><td rowspan=1 colspan=1>1.50D</td></tr><tr><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>Separation between TLOFand FATO perimeters 3</td><td rowspan=1 colspan=1>0.34D</td><td rowspan=1 colspan=1>0.34D</td><td rowspan=1 colspan=1>0.34D</td></tr><tr><td rowspan=1 colspan=1>G</td><td rowspan=1 colspan=1>Safety Area Width</td><td rowspan=1 colspan=1>SeeTable 2-4</td><td rowspan=1 colspan=1>0.42 D but not less than30 ft (9.1 m)</td><td rowspan=1 colspan=1>See Table 2-4</td></tr></table>

See paragraph 2.7.2 for additional guidance.  
See paragraph 2.8.5 for adjustments for heliport elevations above 1000′ MSL.  
Confirm minimum separation between TLOF and FATO is maintained when the TLOF dimensions are adjusted.

## 2.7 Touchdown and Liftoff Area (TLOF).

## 2.7.1 TLOF Location.

TLOFs are located per the following guidelines:

Heliport TLOFs can be located at ground level, on elevated structures, and at rooftop level.

Every heliport will have at least one TLOF. For ground-based or water-based operations (but not rooftop operations), a TLOF can be located within the FATO or outside the FATO. This can be accomplished either over land or over water where the FATO is over the water and the TLOF is on land or is located on a water-based vessel. When the TLOF is located outside of the FATO, provide additional taxi route and/or hover taxi capability. See Figure 3-4.

When the TLOF is located within the FATO, the TLOF is centered within the FATO and along the major axis of the FATO, centered within the load-bearing area (LBA) and designed for dynamic loads.

As an option, TLOFs can be co-located with heliport parking positions outside of the FATO, as shown in Figure 3-4. These TLOFs are designed for static loadbearing. For TLOFs located outside of a FATO, ensure that there are no buildings or other obstacles in the vicinity of the TLOF that could cause turbulence or difficulties with helicopter maneuvering in crosswind conditions.

At a PPR heliport rooftop or other PPR elevated facility, where the entire FATO is not load-bearing, locating the TLOF in an LBA that is as large as possible may provide some operational advantages. Locate the TLOF in the center of the LBA in this case.

## 2.7.2 TLOF Size and Shape.

The TLOF size is a function of the heliport type and controlling dimension D of the design helicopter. A rectangular TLOF may provide the pilot with better alignment cues than a circular shape, but a circular TLOF may be more recognizable in an urban environment. Increasing the TLOF and the size of the LBA centered on the TLOF may provide enhanced safety and operational advantages. See Figure 2-6 and Table 2-1.

## 2.7.2.1 TLOF Size.

The size of the TLOF is shown in Table 2-1. Design considerations include:

For elevated public GENERAL AVIATION heliport and elevated HOSPITAL heliports, if the FATO is not load-bearing, increase the minimum width, length, or diameter of the TLOF to the D of the design helicopter.

At PPR facilities, if only a portion of the TLOF is paved, design the TLOF so the minimum length and width of this paved portion is not less than twice the maximum dimension (length or width) of the

undercarriage of the design helicopter. Locate the center of the TLOF in the center of this paved portion.

For HOSPITAL heliports, the minimum TLOF size is 40 ft × 40 ft (12.2 m × 12.2 m).

At PPR rooftop or elevated facilities, locate the center of the LBA of the TLOF in the center of the FATO when the TLOF is located inside and in the center of the FATO. Design the minimum dimension of the TLOF to be at least the smaller of 0.83 D and twice the maximum dimension (length or width) of the undercarriage of the design helicopter when the following two conditions are:

a. the height of the TLOF surface above the adjacent ground or structure is no greater than 30 inches (0.8 m),

b. there is a solid adjacent ground or structure equal to the OL able to support 20 lbs/square (sq) ft (98 kg/sq m) live load.

Consider the specified facility requirements for heliports where helicopter flight manuals specify the minimum size required for operations.

## 2.7.2.2 TLOF Shape.

For GENERAL AVIATION and HOSPITAL heliports, TLOFs are generally square, rectangular, or circular; however, other shapes may be used.

For TRANSPORT heliports, the TLOF is generally square or rectangular.

## 2.7.3 TLOF Design Loads.

## 2.7.3.1 Static Loads.

Design and construct the TLOF and any load-bearing surfaces to support the weight of the design helicopter and any ground support vehicles, as a minimum. For design purposes, the design static load is equal to the design helicopter’s maximum takeoff weight applied through the total contact area of the wheels or skids. Consult with helicopter manufacturers to obtain the contact area for the specific helicopters of interest.

Loads are applied through the contact area of the tires for wheel-equipped helicopters or the contact area of the skid for skid-equipped helicopters. See Appendix C for helicopter weights, landing gear configurations, and helicopter dimensional data.

## 2.7.3.2 Dynamic Loads.

Design elevated TLOFs, and any TLOF supporting structure, to be capable of supporting the dynamic loads of the design helicopter. See paragraph 2.7.7.2. A dynamic load of 0.2 second or less duration may occur during a hard landing. For design purposes, assume dynamic loads at 150 percent of the takeoff weight of the design helicopter. When specific loading data is not available, assume 75 percent of the weight of the design helicopter is applied equally through the contact area of the rear two wheels (or the pair of rear wheels of a dual-wheel configuration) of a wheel-equipped helicopter. For a skid-equipped helicopter, assume 75 percent of the weight of the design helicopter is applied equally through the aft contact areas of the two skids of a skid-equipped helicopter. (See Figure 2-14.) Contact manufacturers to obtain the aft contact area for specific helicopters of interest.

## 2.7.3.3 Rotor Loads.

Rotor downwash loads are approximately equal to the weight of the helicopter distributed uniformly over the disk area of the rotor. Rotor downwash loads are generally less than the loads specified in building codes for snow, rain, or wind loads typically used in structural design calculations.

## 2.7.4 Ground-level TLOF Pavement and Surface Characteristics.

General surface characteristics and pavement guidelines include:

Provide either a paved or aggregate-turf surface for the TLOF (see AC 150/5370- 10, Standard Specifications for Construction of Airports, Items P-217, Aggregate-Turf Pavement, and P-501, Cement Concrete Pavement).

Use Portland cement concrete (PCC) when feasible for ground-level facilities. An asphalt surface is less desirable for heliports as it may rut under the wheels or skids of a parked helicopter. This has been a factor in some rollover accidents. In addition, sections of asphalt have also been known to adhere to a helicopter’s skids only to fall off after takeoff creating a hazard to vehicles, buildings, and persons on the ground.

Use a roughened (broomed) pavement finish to provide a skid-resistant surface for helicopters and non-slippery footing for people.

Design the paved portion to dynamic load bearing where only a portion of the TLOF is paved for PPR heliports. Design the adjacent ground or structure of the TLOF for the static loads of the design helicopter.

To avoid unstable risk factors such as dynamic rollovers, match the transition elevations between the paved and unpaved portions of the TLOF.

Provide a 10-foot-wide rapid runoff shoulder at a negative 3-5% grade.

## 2.7.5 Ground-level TLOF Gradients.

To ensure positive drainage of the entire TLOF area, design the TLOF to have a negative gradient between 0.5 percent and 2 percent for GENERAL AVIATION and HOSPITAL heliports. For TRANSPORT heliports, design the TLOF to have a longitudinal gradient between 0.5 and 1 percent and a transverse gradient between 0.5 and 1.5 percent. Grade the entire TLOF to provide positive drainage. In addition, slope grades away from ingress/egress areas and emergency exits. See Figure 2-7.

Figure 2-7. Heliport Gradients and Rapid Runoff Shoulder - Load-bearing FATOs  
![3784c1a85c9f24effe3d9fbb9faffa9b0d3d3d7e49c13dc4e8de2a781bcc4c08.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3784c1a85c9f24effe3d9fbb9faffa9b0d3d3d7e49c13dc4e8de2a781bcc4c08.jpg)  
See paragraph 2.7.5 for specific gradient standards for HOSPITAL, GENERAL AVIATION, and TRANSPORT heliports.  
The slope direction is based on the topography of the site.  
Grade the TLOF, FATO, and safety area to provide positive drainage of the entire area for the TLOF, FATO, and safety area.  
Stabilize FATO non-load-bearing surfaces.

## 2.7.6 Elongated TLOF and FATO.

2.7.6.1 Where space allows, an elongated TLOF and FATO can be provided to enhance safety and operational flexibility. This enhanced safety is particularly relevant during emergency landings as the elongated TLOF provides a longer TLOF area and longer FATO area for approach and landing. This configuration also provides enhanced obstruction clearance both longitudinally (along the approach/departure surfaces) and laterally (due to the longer transitional surfaces).

2.7.6.2 As an option, design an elongated TLOF with a landing position in the center and two takeoff positions, one at either end. If the TLOF is elongated, also provide an elongated FATO. See Figure 2-8 and Table 2-2 for the layout dimensions of an elongated FATO.

Figure 2-8. Optional Elongated TLOF and FATO with Two Takeoff Positions  
![e8b3e3ac02c993912bbc6d054ca2fb5e01b48d333ebccd3a5abb1e22d1dbda09.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/e8b3e3ac02c993912bbc6d054ca2fb5e01b48d333ebccd3a5abb1e22d1dbda09.jpg)  
For a circular TLOF and FATO, dimensions A, B, C, and E refer to diameters.

Table 2-2. Minimum Dimensions for Elongated FATO with Two Takeoff Positions
<table><tr><td rowspan=1 colspan=1>Dim</td><td rowspan=1 colspan=1>Item</td><td rowspan=1 colspan=1>GA</td><td rowspan=1 colspan=1>TRANSPORT</td><td rowspan=1 colspan=1>HOSPITAL</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>TLOF Width</td><td rowspan=1 colspan=1>0.83D</td><td rowspan=1 colspan=1>0.83 D but not less than50 ft (15.2 m)</td><td rowspan=1 colspan=1>0.83 D but not less than40 ft (12.2 m)</td></tr><tr><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>TLOF/LandingPosition Length</td><td rowspan=1 colspan=1>0.83D</td><td rowspan=1 colspan=1>0.83 D but not less than50 ft (15.2 m)</td><td rowspan=1 colspan=1>0.83 D but not less than40 ft (12.2 m)</td></tr><tr><td rowspan=1 colspan=1>C</td><td rowspan=1 colspan=1>FATO Width</td><td rowspan=1 colspan=1>1.25 D</td><td rowspan=1 colspan=1>1.66 D but not less than100 ft (30.5 m)</td><td rowspan=1 colspan=1>1.25D</td></tr><tr><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>Separation Betweenthe TLOF and FATO</td><td rowspan=1 colspan=1>0.34D</td><td rowspan=1 colspan=1>0.34D</td><td rowspan=1 colspan=1>0.34D</td></tr><tr><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>Safety Area Width</td><td rowspan=1 colspan=1>See Table 2-4</td><td rowspan=1 colspan=1>0.42 D but not less than50 ft (15.2 m)</td><td rowspan=1 colspan=1>See Table 2-4</td></tr></table>

## 2.7.7 Rooftop and Other Elevated TLOFs and FATOs.

## 2.7.7.1 Elevation and Configuration of Rooftop and other Elevated Heliports.

Table 2-3 provides design parameters related to elevation, obstacles, and edge restraints for rooftop and other elevated TLOFs and FATOs.

Table 2-3. TLOF Elevation and Configuration of Rooftop and other Elevated Heliports
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>GA</td><td rowspan=1 colspan=1>TRANSPORT</td><td rowspan=1 colspan=1>HOSPITAL</td></tr><tr><td rowspan=1 colspan=1>Elevation</td><td rowspan=1 colspan=1>TLOF elevation is abovethe elevation of theFATO</td><td rowspan=1 colspan=1>FATO and TLOFelevations are both abovethe elevation of theadjacent safety area</td><td rowspan=1 colspan=1>TLOF elevation is abovethe elevation of theFATO</td></tr><tr><td rowspan=1 colspan=1>Obstacles</td><td rowspan=1 colspan=1>Construct the TLOFabove the level of anyobstacle in the FATO andsafety area that cannot be|removed</td><td rowspan=1 colspan=1>Construct the FATOabove the level of anyobstacle in the safety area|that cannot be removed</td><td rowspan=1 colspan=1>Construct the TLOFabove the level of anyobstacle in the FATO andsafety area that cannot beremoved</td></tr><tr><td rowspan=1 colspan=1>Edgerestraints</td><td rowspan=1 colspan=1>N/A</td><td rowspan=1 colspan=1>N/A</td><td rowspan=1 colspan=1>Edge restraints ofminimal height (no higherthan 4 inches (102 mm))on ramps may projectabove the elevation of theedge of the TLOF</td></tr></table>

See Figure 2-9 and Figure 2-10 for elevated heliport configurations.

Figure 2-9. Elevated Heliport: GENERAL AVIATION and HOSPITAL  
![deb6f61d96c3e2d95b9e1d38f72c934acbee0ae5f017dd07dc4e7f3fae39b939.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/deb6f61d96c3e2d95b9e1d38f72c934acbee0ae5f017dd07dc4e7f3fae39b939.jpg)  
See Figure 4-9 for safety net and lighting details.

Figure 2-10. Elevated Heliport: TRANSPORT  
![63b669491a157f98d231f8ab1f94859a6fbb2faf9671b783b0f46a34b29487f1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/63b669491a157f98d231f8ab1f94859a6fbb2faf9671b783b0f46a34b29487f1.jpg)  
See Figure 4-9 for safety net and lighting details.

## 2.7.7.2 Elevated TLOF Design Loads.

Design elevated TLOFs, and any TLOF supporting structure, to be capable of supporting the dynamic loads of the design helicopter, described in paragraph 2.7.3.2 and Figure 2-14.

For TRANSPORT heliports, design both the TLOF and FATO, and any supporting structures, for the TLOF and FATO to be capable of supporting the dynamic loads of the design helicopter.

## 2.7.7.3 Elevated TLOF Surface Characteristics.

Construct rooftop and other elevated heliport TLOFs of aluminum, metal, or concrete (or other materials subject to local building codes).

Use a finish for TLOF surfaces that provides a skid-resistant surface for helicopters and non-slippery footing for people.

For TRANSPORT heliports, the surface characteristics described above apply to both the TLOF and FATO.

## 2.7.7.4 Access to Elevated TLOFs and Elevated FATOs.

Title 29 CFR Part 1926.34, Means of Egress, requires two separate access points for an elevated structure such as an elevated TLOF or FATO. Guidelines for access design include:

Design stairs in compliance with 29 CFR Part 1910.25, Stairways.

Design handrails described in this regulation to fold down or be removable to below the level of the TLOF or FATO so they will not be hazards during helicopter operations.

For HOSPITAL heliports, provide access to and from the TLOF via a ramp to provide for quick and easy transportation of a patient on a gurney. Build ramps in accordance with state and local requirements. Design the width of the ramp, and any turns in the ramp, to be wide enough to accommodate a gurney with a person walking on each side. Design straight segments of the ramp to be at least 6 feet (1.8 m) wide. Additional width may be required in the turns. Provide the ramp with a slip-resistant surface.

## 2.7.7.5 Elevated Heliport Design Considerations.

## 2.7.7.5.1 Obstructions.

Elevator penthouses, cooling towers, exhaust vents, fresh-air vents, and other elevated features can affect heliport operations. Establish control mechanisms to ensure obstruction hazards are not installed after the heliport is operational.

## 2.7.7.5.2 Air Quality.

Helicopter engine exhaust can affect building air quality if the heliport is too close to fresh air vents. When designing a building intended to support a helipad, locate fresh air vents to mitigate impacts on building air quality. When adding a heliport to an existing building, relocate fresh air vents, if necessary, or if relocation is not practical, install charcoal filters or a fresh air intake bypass louver system for heating, ventilation, and air conditioning (HVAC) systems or implement other measures as needed.

## 2.8 Final Approach and Takeoff Area (FATO).

A heliport has at least one FATO. The FATO typically contains a TLOF within its borders at which arriving helicopters terminate their approach and from which departing helicopters take off.

## 2.8.1 FATO Minimum Width, Length (or Diameter).

Design the FATO per the following guidelines:

Design the FATO and the safety area to be square or rectangular if the TLOF is square or rectangular, respectively.

Design the FATO and the safety area to be round if the TLOF is round.

The long axis of a rectangular FATO is aligned with the preferred flight path.

The minimum width and length of the FATO are shown in Table 2-1 for all three types of heliports.

See Figure 2-6 for a depiction of the relationship of the TLOF to the FATO and the safety area.

Design the distance between the TLOF, FATO, and safety area perimeters to be equidistant regardless of the shape of the TLOF.

For HOSPITAL heliports, locate the FATO to provide ready access to the hospital’s emergency room or to the intended destination for the patient.

At PPR heliports, the operator and heliport owner ensure all pilots using the facility are thoroughly knowledgeable with all facility limitations when the operator of a PPR heliport chooses not to provide additional FATO length.

## 2.8.2 FATO Load-bearing Capacity – Ground-level Heliports.

For both standard shaped FATOs and extended/elongated FATOs, the FATO outside the TLOF need not be load-bearing if the heliport operator marks the TLOF as load-bearing. This guidance applies to standard FATO shapes, or elongated or extended FATOs.

For GENERAL AVIATION and PPR heliports, if the heliport operator does not mark the TLOF and/or intends that the helicopter be able to land anywhere within the FATO, design the FATO outside the TLOF, and any FATO supporting structure (like the TLOF) to be capable of supporting the dynamic loads of the design helicopter, as described in paragraph 2.7.3.2.

## 2.8.3 FATO Ground-level Surface Characteristics.

Design the edge of the FATO abutting the TLOF to be at the same elevation as the TLOF. Treat the FATO to prevent loose stones and any other flying debris caused by rotor downwash, if the FATO is unpaved.

## 2.8.4 FATO Gradients.

## 2.8.4.1 Load-bearing FATO.

Design a load-bearing FATO to have a negative gradient between 0.5 percent and 5 percent away from the edge of the TLOF. Design a negative gradient of not more than 2 percent in any areas where a helicopter is expected to land. To ensure TLOF drainage, design gradients of rapid runoff shoulders to be between 3 and 5 percent. In addition, slope grades away from ingress/egress areas and emergency exits. See Figure 2-7.

## 2.8.4.2 Non-load-bearing FATO.

When the FATO is non-load-bearing and/or not intended for use by the helicopter, there are no specific requirements for the gradient of the

FATO. In this case, design the gradient to be negative 5 percent (-5%) or more to ensure adequate drainage away from the TLOF. However, stabilize non-load-bearing surfaces.

## 2.8.5 FATO Additional Length for Higher Elevations.

At elevations above 1000 feet (305 m) MSL, a longer FATO provides an increased safety margin and greater operational flexibility. For ground-level heliports, provide the additional FATO length required, as shown in Figure 2-11. Design the minimum distance between the TLOF perimeter and the FATO perimeter to be no less than 0.34 D of the design helicopter to provide an increased safety margin and greater operational flexibility.

For elevated heliports above 1000 feet (305 m) MSL, performance characteristics of helicopters using the facility may be considered in lieu of, or in conjunction with, an additional FATO length, in particular related to Hover-Out-of-Ground Effect (HOGE) capability.

Figure 2-11. Additional FATO Length for Heliports at Higher Elevations  
![ff7547d3c926863155df65f595ca33dc3408f9c1b4651262f282ab0cb2b7bf10.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ff7547d3c926863155df65f595ca33dc3408f9c1b4651262f282ab0cb2b7bf10.jpg)

## 2.8.6 Rooftop and Other Elevated FATOs.

## 2.8.6.1 Design Loads.

Design elevated FATOs, and any FATO supporting structure, to be capable of supporting the dynamic loads of the design helicopter. See paragraph 2.7.3.2.

There are some helicopter performance benefits and increased operational flexibility if the FATO outside the TLOF is load-bearing. Design the FATO outside of the TLOF to be load-bearing or, as an option, increase the minimum width and length, or diameter of the TLOF, to the controlling dimension D of the design helicopter.

## 2.8.6.2 Elevation.

Elevate the FATO and TLOF above the level of any object in the safety area that cannot be removed.

## 2.8.6.3 FATO Extension into Clear Airspace.

As an option, where the FATO is non-load bearing, design the FATO outside the TLOF to extend into clear airspace for elevated heliports. Where space is available, portions of the FATO may share the rooftop for increased operational flexibility and helicopter performance benefits.

For elevated PPR heliports, consider the following:

a. As an option for elevated PPR heliports, design the FATO outside the TLOF and the safety area to extend into the clear airspace for elevated PPR heliports, if the heliport operator intends to mark the TLOF.

b. If the heliport operator does not mark the TLOF and/or intends that the helicopter be able to land anywhere within the FATO, design the FATO outside the TLOF and any FATO supporting structure (including the TLOF), to support the dynamic loads of the design helicopter.

c. As an option, increase the LBA length and width (or diameter, if a circle) without a corresponding increase in the size of the FATO.

FATOs can extend over water, as shown in Figure 2-12. In addition, FATOs can be located over water with associated TLOFs located on land. See Figure 3-4.

## 2.8.6.4 FATO Only Area.

A FATO can be established at a heliport for common-use approaches and departures only and would not include a TLOF within the FATO. In this case, one or more TLOFs would be located outside of the FATO, as described in paragraph 2.7 and shown in Figure 3-4.

## 2.8.6.5 Elevated Surface Characteristics.

Construct rooftop and other elevated heliport FATOs of metal, concrete, or other materials subject to local building codes. Provide the FATO surface with non-slippery footing for people.

## 2.8.6.6 Safety Net.

Construct safety nets, as described in paragraph 2.10.

## 2.8.6.7 Access to Elevated FATOs.

Provide access, as described in paragraph 2.7.7.4.

## 2.8.6.8 Fixed and Mobile Objects within the FATO.

The FATO design standards of this AC assume the TLOF and FATO are closed to other aircraft if a helicopter or other mobile object is within the FATO or the safety area. Remove all fixed objects projecting above the FATO elevation except for lighting fixtures, which may project a maximum of 2 inches (51 mm) and must be frangible. For ground-level heliports, remove all above-ground objects to the extent practicable.

## 2.8.6.9 FATO/FATO Separation.

Simultaneous landings or takeoffs may be authorized if the distance between the landing or takeoff points is at least 200 feet (61 m) and the courses to be flown do not conflict. Refer to surface markings to determine the 200-foot minimum.

## 2.9 Safety Area.

A safety area surrounds a FATO, as shown in Figure 2-1. The minimum safety area dimensions are provided in Table 2-1 for TRANSPORT heliports. For GENERAL AVIATION, HOSPITAL, and PPR heliports, the safety area width is the same on all sides and is a function of heliport marking scenarios, as shown in Table 2-4.

Table 2-4. Minimum VFR Safety Area Width as a Function of Heliport Markings GENERAL AVIATION, HOSPITAL, and PPR Heliports
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Scenario 1</td><td rowspan=1 colspan=1>Scenario 2</td><td rowspan=1 colspan=1>Scenario 3</td><td rowspan=1 colspan=1>Scenario 4</td></tr><tr><td rowspan=1 colspan=1>TLOF perimeter marked</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td></tr><tr><td rowspan=1 colspan=1>FATO perimeter marked</td><td rowspan=1 colspan=1>See Note</td><td rowspan=1 colspan=1>See Note</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td></tr><tr><td rowspan=1 colspan=1>Standard &quot;H&quot; &#x27; marking</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>No</td></tr><tr><td rowspan=1 colspan=1>Safety area widthGENERAL AVIATIONheliports</td><td rowspan=1 colspan=1>0.28 D butnot less than20 ft (6.1 m)</td><td rowspan=1 colspan=1>0.28 D butnot less than30 ft (9.1 m)</td><td rowspan=1 colspan=1>0.50 D butnot less than20 ft (6.1 m)</td><td rowspan=1 colspan=1>0.50 D butnot less than30 ft (9.1 m)</td></tr><tr><td rowspan=1 colspan=1>Safety area widthHOSPTIAL and PPRheliports</td><td rowspan=1 colspan=1>0.28 D butnot less than10 ft (3 m)</td><td rowspan=1 colspan=1>0.28 D butnot less than20 ft (6.1 m)</td><td rowspan=1 colspan=1>0.50 D butnot less than20 ft (6.1 m)</td><td rowspan=1 colspan=1>0.50D butnot less than30 ft (9.1 m)</td></tr><tr><td rowspan=1 colspan=5>Note: Scenarios 1 and 2 apply whether the FATO is not marked or not. Do not mark the FATO if (a) the FATO (or part of the FATO) is a non-load-bearing surface and/or (b) the TLOF iselevated above the level of a surrounding load-bearing area.</td></tr></table>

## 2.9.1 Fixed and Mobile Objects within the Safety Area.

The Safety Area design standards of this AC assume the TLOF and FATO are closed to other aircraft if a helicopter or other mobile object is within the FATO or the safety area. Remove all fixed objects within the Safety Area projecting above the FATO elevation except for lighting fixtures, which may project a maximum of 2 inches (51 mm) and must be frangible. For ground-level heliports, remove all above-ground objects to the extent practicable.

## 2.9.2 Safety Area Surface.

Guidelines on surface characteristics of safety areas include:

The safety area need not be load-bearing.

Design the safety area abutting the FATO at the same elevation as the FATO to avoid the risk of catching a helicopter skid or wheel.

Clear the safety area of flammable materials and treat the area to prevent loose stones and any other flying debris caused by rotor wash.

Safety areas can extend over water, as shown in Figure 2-12 and Figure 2-13.

## 2.9.3 Safety Area Gradients.

Design the surface of the safety area to be no steeper than a downward slope of 2:1 (2 units horizontal in 1 unit vertical). In addition, design the safety area elevation to be at or below the FATO edge elevation. See Figure 2-7.

Figure 2-12. Non-load-bearing FATO and Safety Area over Water: GENERAL AVIATION and HOSPITAL Heliports  
![9d6fd22e83720bcded804684914bebadfbc83d6178fcffa048fd7e433179d17d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9d6fd22e83720bcded804684914bebadfbc83d6178fcffa048fd7e433179d17d.jpg)

Figure 2-13. Non-load-bearing Safety Area over Water: TRANSPORT  
![67b6deee49aa9670c3dd4937467b2f48076f290ebac1d8e93a291835906bdadc.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/67b6deee49aa9670c3dd4937467b2f48076f290ebac1d8e93a291835906bdadc.jpg)  
See paragraph 2.7 and Figure 3-4 for guidance on a TLOF located outside of the FATO.

## 2.10 Fall Protection and Safety Net Design.

Design heliport safety nets as follows:

Title 29 CFR Part 1910.23, Guarding Floor and Wall Openings and Holes, requires the provision of fall protection if the platform is elevated 4 feet (1.2 m) or more above its surroundings. The FAA recommends such protection for all platforms elevated 30 inches (0.8 m) or more.

Do not use permanent railings or fences since they would be safety hazards during helicopter operations.

Install a safety net meeting state and local regulations but not less than 5 feet (1.5 m) wide as an option.

Fasten both the inside and outside edges of the safety net to a solid structure.

Construct nets of materials that are resistant to environmental effects.

Table 2-5 describes the differences in safety net design for rooftop and other elevated heliports.

Table 2-5. Differences in Safety Net Design for Rooftop and Elevated Heliports
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>GA</td><td rowspan=1 colspan=1>TRANSPORT</td><td rowspan=1 colspan=1>HOSPITAL</td></tr><tr><td rowspan=1 colspan=1>Load</td><td rowspan=1 colspan=1>Design the safety net tohave a load carryingcapability of 25 1bs/sq ft(122 kg/sq m)</td><td rowspan=1 colspan=1>Design the safety net tohave a load carryingcapability of 50 1bs/sq ft(244 kg/sq m)</td><td rowspan=1 colspan=1>Design the safety net tohave a load carryingcapability of 25 lbs/sq ft(122 kg/sq m)</td></tr><tr><td rowspan=1 colspan=1>Elevation</td><td rowspan=1 colspan=1>Design the safety net tobe at or below theelevation of the TLOF</td><td rowspan=1 colspan=1>Design the safety net tobe at or below theelevation of the FATO</td><td rowspan=1 colspan=1>Design the safety net tobe at or below theelevation of the TLOF</td></tr></table>

See Figure 4-9 for safety net characteristics.

## 2.11 Pavement Design and Soil Stabilization.

Pavements distribute a helicopter’s weight over a larger area of the subsurface, as well as provide a water-impervious, skid-resistant wearing surface. See Figure 2-14 and paragraph 2.7.3 for guidance on design loads.

Pave TLOFs, FATOs, taxiways, and parking aprons to improve their load carrying ability, minimize the erosive effects of rotor wash, and facilitate surface runoff.

PCC pavement is preferred over asphalt pavement for areas used for helicopter operations, wherever practical.

Stabilize turf areas on heliports subject to rotor downwash (including unpaved FATOs, unpaved taxiway shoulders, and other unpaved areas as needed), so these areas will not be subject to erosion or damage from rotor downwash due to helicopter operations.

In some instances, loads imposed by ground support vehicles may exceed those of the largest helicopter expected to use the facility and may require additional pavement thickness.

Thicker pavements may be needed to support heavier helicopters or where the quality of the subsurface soil is poor or questionable.

Find guidance on pavement design and soil stabilization in AC 150/5320-6, Airport Pavement Design and Evaluation, and AC 150/5370-10 at the FAA Airports website (https://www.faa.gov/airports).

Figure 2-14. Helicopter Landing Gear Loading: Gradients and Pavement  
![0071e43ddf90fdf8be62b9f6ea655232b9a48932ece7da11cf4e73e93dbb6585.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0071e43ddf90fdf8be62b9f6ea655232b9a48932ece7da11cf4e73e93dbb6585.jpg)

## 2.11.1 Soil Stabilization.

Use appropriate methods of soil stabilization to meet different site requirements. Consider helicopter weight, ground support vehicle weight, operational frequency, soil analysis, and climatic conditions in selecting the method(s) and extent of surface stabilization.

## 2.11.1.1 Turf.

A well-drained and well-established turf that presents a smooth, dense surface is usually the most cost-effective surface stabilization available. In some combinations of climates and weather conditions, turf surfaces can support the weight of many of the smaller helicopters for low frequency use by private and corporate operators during much of the year. Turf surfaces also provide reasonable protection against wind, rotor wash, or water erosion. Climatic and soil conditions dictate the appropriate grass species to use at the site. Find guidance on turf establishment in AC 150/5370-10.

## 2.11.1.2 Aggregate Turf.

Where heliports are located on soils that have poor load-carrying capabilities when wet, consider overcoming this deficiency by mixing selected granular materials into the upper 12 inches (0.3 m) of the soil. Suitable granular materials for this purpose are crushed stone, pit-run gravel, coarse sand, or oyster shells. Use a sufficient ratio of aggregate to soil to improve the stability of the soil yet retain the soil’s ability to support grass. For additional guidance, see Item 217 of AC 150/5370-10.

## 2.11.2 Formed Masonry Shapes and Other Materials.

Precast masonry shapes vary in size and shape from a brick paver to an open block. Lay pavers on a prepared bed to present a solid surface. Embed precast blocks in the soil with grass growing in the natural openings. Architectural catalogs identify different masonry shapes that are commercially available for this purpose. Other materials such as pre-manufactured concrete or newer materials may be used where applicable.

## 2.11.3 Pierced Metal Panels.

Lay perforated metal panels that may allow grass to grow through the openings on the ground to provide a hard surface for helicopter operations. Engineering catalogs identify commercially available panels.

## 2.12 VFR Approach/Departure Paths.

The approach/departure and transitional surfaces provide enough airspace clear of hazards to allow safe approaches to, and departures from, the FATO. Figure 2-15 and Figure 2-16 show these surfaces for straight-in and curved approaches, respectively. Note that VFR approach/departure sectored airspace can be used to provide increased approach/departure airspace and enhanced obstacle clearance surfaces for helicopter approaches and departures. Sectored airspace can provide helicopter pilots with greater flexibility and enhanced safety, particularly in areas with mountains or nearby obstructions (e.g., buildings), or heliports in areas with variable wind conditions.

Figure 2-15. VFR Heliport Approach/Departure and Transitional Surfaces  
![9e8e5b29c1db6473fd6c1ed2ea397c04e07fc5633600f560ea051e947c06134e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9e8e5b29c1db6473fd6c1ed2ea397c04e07fc5633600f560ea051e947c06134e.jpg)

Figure 2-16. VFR Curved Approach/Departure and Transitional Surfaces – GENERAL AVIATION and TRANSPORT Heliports  
![0c2182010b7f2f7c28de3800679dae8a370febdd46bc2a18b517707213bd792e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0c2182010b7f2f7c28de3800679dae8a370febdd46bc2a18b517707213bd792e.jpg)  
Use any combination of straight portions of one curved portion using the following formula: S + R ≥ 1,886 ft (575 m) and R ≥ 886 ft (270 m), where S is the length of the straight portion(s) and R is the radius of the turn. Note that any combination ≥ 1,886 ft (575 m) will work.  
The minimum total length of the centerline of the straight and curved portion is 4,000 ft (1,219 m).  
Helicopter takeoff performance may be reduced in a curve. Consider a straight portion along the takeoff climb surface prior to the start of the curve to allow for acceleration.

## 2.12.1 Number of Approach/Departure Paths.

Develop heliport approach/departure paths per the following guidelines:

Align preferred approach/departure paths with the predominant wind direction so downwind operations are avoided and crosswind operations are kept to a minimum.

To accomplish this, design a heliport to have several approach/departure paths or sector approach/departure paths. This ability is especially important for TRANSPORT heliports.

Base additional approach/departure paths on the assessment of the prevailing winds and surrounding obstructions. When wind data is not available, separate additional flight paths and the preferred flight path by at least (but not limited to) 135 degrees. See Figure 2-15.

A second flight path provides an additional safety margin and operational flexibility for variable wind conditions. If it is not feasible to provide complete coverage of wind conditions through multiple approach/departure paths, operational limitations may be necessary under certain wind conditions. See paragraph 1.9.1.

At a PPR heliport that has only one approach/departure path, the heliport operator ensures all pilots using the facility are thoroughly knowledgeable with the approach/departure path, and any other facility limitations specific to this PPR heliport.

## 2.12.2 VFR Approach/Departure and Transitional Surfaces.

Figure 2-15 illustrates the approach/departure surfaces and transitional surfaces. Develop these heliport surfaces per the following guidelines:

An approach/departure surface is centered on each approach/departure path. The approach/departure path starts at the outer edge of the FATO and slopes upward at 8:1 (8 units horizontal in 1 unit vertical) for 4,000 feet (1,219 m) where the width is 500 feet (152 m) at a height of 500 feet (152 m) above the heliport elevation.

The transitional surfaces start from the edges of the FATO parallel to the flight path centerline, and from the outer edges of the 8:1 approach/departure surface and extend outwards at a slope of 2:1 (2 units horizontal in 1 unit vertical) for 250 feet (76 m) from the centerline. The transitional surfaces extend longitudinally from the edge of the FATO to the far end of the approach/departure surface. The transitional surface does not apply to the FATO edge opposite the approach/departure surface. See Figure 2-15.

Clear the approach/departure and transitional surfaces of penetrations unless an FAA aeronautical study determines such penetrations not to be hazards. The FAA conducts such aeronautical studies only at public heliports, heliports operated by a federal agency or the DoD, and private heliports. Paragraph 1.11 provides additional information on hazards to air navigation.

At HOSPITAL and PPR heliports, consider implementation of lateral extensions as an option per the following guidelines:

a. Increase the width of the 8:1 approach/departure surface for a distance of 2,000 feet (610 m) by adding lateral extensions, as shown in Figure 2-17.

b. The lateral extensions on each side of the 8:1 approach/departure surface start at the width of the FATO and are increased so that at 2,000 feet (610 m) from the FATO they are 100 feet (30.5 m) wide.

c. Ensure that obstacles do not penetrate both Area A and Area B, unless the FAA determines that the penetration is not a hazard. Mark or light all such penetrations. See paragraph 1.11 for more information on hazard determinations.

Figure 2-17. VFR HOSPTIAL and PPR Heliport Optional Lateral Extensions of the 8:1 Approach/Departure Surface  
![0721679ce460447a793b346fa62eec702fd1f3df8b95a4a93cec33b013dbf7d5.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0721679ce460447a793b346fa62eec702fd1f3df8b95a4a93cec33b013dbf7d5.jpg)  
Allow penetration(s) of Area A or Area B lateral extensions but not both, provided that obstacles are marked or lighted and obstacles are not determined to be a hazard by the FAA.

## 2.12.3 Curved VFR Approach/Departure Paths.

2.12.3.1 Figure 2-16 shows curved approach/departure surfaces for GENERAL AVIATION and TRANSPORT heliports. Figure 2-18 shows curved approach/departure surfaces for HOSPITAL and PPR heliports.

2.12.3.2 Develop heliport curved VFR approach/departure paths per the following guidelines:

When including a curved portion in the approach/departure path, confirm the sum of the radius of the arc defining the centerline and the length of the straight portion originating at the FATO is not less than 1,886 feet (575 m).

Design the approach/departure path so the minimum radius of the curve is 886 feet (270 m) and that the curve follows a 1,000-foot (305 m) straight section.

Design the approach/departure path so the combined length of the centerline of the curved portion and the straight portion is 4,000 feet (1,219 m).

For HOSPITAL and PPR heliports, consider use of lateral extensions, as described in paragraph 2.12.2 subparagraph 4.

As an option, include one curve in VFR approach/departure paths.

As an option, design these paths to use the airspace above public lands, such as freeways, railroads, lakes, or rivers.

## 2.12.4 Flight Path Alignment Guidance.

As an option, use flight path alignment markings and/or flight path alignment lights where it is desirable and practicable to indicate approach and/or departure flight path direction(s). See Figure 2-19 and paragraph 4.8.

## 2.12.5 Periodic Review of Obstructions.

Heliport owners and operators should re-examine obstacles near approach/departure paths, at least annually, to prevent the encroachment of hazards. This re-examination includes an appraisal of tree growth near approach and departure paths. Paragraph 1.11 provides additional information on hazards to air navigation. Pay attention to obstacles that need to be marked or lighted. It may be helpful to maintain a list of the GPS coordinates and the top (highest) elevation of obstacles.

Figure 2-18. VFR HOSPITAL and PPR Heliport Optional Lateral Extension of the Curved 8:1 Approach/Departure Surface  
![db8fcb810d450fd629454345c1cb6cb2bae22f32c5fc3871d73319a9433f25b5.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/db8fcb810d450fd629454345c1cb6cb2bae22f32c5fc3871d73319a9433f25b5.jpg)  
The approach surface may consist of one curved portion preceded and/or followed by one straight portion such that: S + R ≥ 1,886 ft (575 m) and R ≥ 886 ft (270 m), where S is the length of the straight portion(s) and R is the radius of the turn. Note that any combination ≥ 1,886 ft (575 m) will work.  
The minimum total length of the centerline of the straight and curved portion is 4,000 ft (1,219 m).  
Helicopter takeoff performance may be reduced in a curve. Consider a straight portion along the takeoff climb surface prior to the start of the curve to allow for acceleration.  
Allow penetration(s) of Area A or Area B lateral extensions but not both, provided that obstacles are marked or lighted and obstacles are not determined to be a hazard by the FAA.

Figure 2-19. Flight Path Alignment Marking and Lights  
![2bad60c8248e7c5ad22364d7bda01f66246c121a665e7e0b190e841980bce623.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2bad60c8248e7c5ad22364d7bda01f66246c121a665e7e0b190e841980bce623.jpg)  
Arrowheads have constant dimensions.  
If necessary, adjust stroke length to match length available. Minimum length = 10 ft (3 m).  
Light type: omnidirectional green lights, Type L-860H or Type L-852H.  
If necessary, locate the lights outside of the arrow.  
In-pavement flight path alignment lighting is recommended.  
See paragraph 4.8 for guidance on flight path alignment markings.

## 2.13 Heliport Protection Zone (HPZ).

The FAA recommends the establishment of an HPZ for each approach/departure surface. The HPZ is intended to enhance the protection of people and property on the ground. This is achieved through heliport owner control over the HPZ. In urban areas where space may be limited, the FAA encourages the heliport owner to control the maximum HPZ area practical. The FAA discourages residences and places of public assembly in an HPZ. (Churches, schools, hospitals, office buildings, parking lots, shopping centers, and other uses with similar concentrations of persons typify places of public assembly.) HPZ dimensions and recommendations include:

The HPZ is the area under the 8:1 approach/departure surface starting at the FATO perimeter and extending out for a distance of 280 feet (85 m) for GENERAL AVIATION and HOSPITAL heliports and a distance of 400 feet (122 m) for TRANSPORT heliports. See Figure 2-20.

The heliport owner should periodically evaluate and clear the HPZ of incompatible objects and activities.

Do not locate hazardous materials, including fuel, compressed oxygen, or other hazardous materials, within the HPZ.

## 2.14 Wind Cone.

## 2.14.1 Specification.

Install a wind cone conforming to AC 150/5345-27, Specification for Wind Cone Assemblies, to show the direction and magnitude of the wind. Use a color that provides the best possible contrast to its background.

## 2.14.2 Wind Cone Location.

Locate the wind cone to provide pilots with valid wind direction and speed information near the heliport under all wind conditions. See AC 150/5340-30, Design and Installation Details for Airport Visual Aids, for installation details. Follow these guidelines for wind cone location:

At many landing sites, there may be no single, ideal location for the wind cone. At other sites, it may not be possible to site a wind cone at the ideal location. In such cases, install more than one wind cone to provide pilots with all the wind information needed for safe operations.

Place the wind cone so pilots on the approach path can see it clearly when the helicopter is 500 feet (152 m) from the TLOF.

Place the wind cone so pilots can see it from the TLOF.

To avoid presenting an obstruction hazard, locate the wind cone(s) outside the safety area, and so it does not penetrate the approach/departure or transitional surfaces.

## 2.14.3 Wind Cone Lighting.

At a heliport intended for night operations, illuminate the wind cone, either internally or externally, to ensure it is clearly visible.

Figure 2-20. Heliport Protection Zone (HPZ)  
![faa6e4a5032bd8b86bc2120a85a763ac4321fa1b8ee7cf4300a0e3dcccfc1b73.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/faa6e4a5032bd8b86bc2120a85a763ac4321fa1b8ee7cf4300a0e3dcccfc1b73.jpg)  
The approach surface starts at the edge of the FATO.  
The length of the Heliport Protection Zone is 400 ft (122 m) for TRANSPORT heliports and 280 ft (85 m) for GENERAL AVIATION and HOSPITAL heliports.  
See paragraph 2.12 for approach surface dimensions.  
See paragraph 2.13 for specific HPZ recommendations.

## CHAPTER 3. Heliport Taxiways, Taxi Routes, and Helicopter Parking

## 3.1 General.

This chapter provides guidance on heliport taxiways, taxi routes, and helicopter parking.

## 3.2 Taxiways and Taxi Routes.

Taxiways and taxi routes provide for the movement of helicopters from one part of a landing facility to another. They provide a connecting path between the FATO and a parking area. They also provide a maneuvering lane within the parking area. General guidance includes:

A taxi route includes the taxiway plus the appropriate clearances needed on both sides.

The configurations of taxiways are illustrated in Figure 3-1, Figure 3-2, and Figure 3-3 for both paved and unpaved taxiways.

At heliports with no parking or refueling area outside the TLOF(s), it is not necessary to provide a taxi route or taxiway.

## 3.3 Taxiway/Taxi Route Widths.

The dimensions of taxiways and taxi routes are a function of helicopter size, taxiway/taxi route marking, and type of taxi operations (ground taxi versus hover taxi). These dimensions are shown in Table 3-1. Normally, the requirement for hover taxi dictates the taxiway/taxi route widths. Consider the following guidelines when designing taxiway/taxi routes:

1. When the fleet comprises a combination of large ground taxiing helicopters and smaller air taxiing helicopters, the larger aircraft may dictate the taxiway/taxi route widths.

2. If wheel-equipped helicopters taxi with wheels not touching the surface, design the facility with hover taxiway widths rather than ground taxiway widths.

3. Where the visibility of the centerline marking cannot always be guaranteed, such as locations where snow or dust commonly obscure the centerline marking, and it is not practical to remove it, determine the minimum taxiway/taxi route dimensions as if there was no centerline marking.

4. Where the TLOF is located outside of the FATO, and aircraft access the TLOF after approaching and hovering at FATO, provide an air taxiway between the FATO and TLOF. See Figure 3-4.

Figure 3-1. Taxiway/Taxi Route Relationship – Paved Taxiway  
![2ff59ed1882e2bb9f090bab65b68b56164538784e6d6fb19a4788e0804583fd3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2ff59ed1882e2bb9f090bab65b68b56164538784e6d6fb19a4788e0804583fd3.jpg)  
See Table 3-1 for taxiway/taxi route width.

Figure 3-2. Taxiway/Taxi Route Relationship – Unpaved Taxiway with Elevated Retroreflective Edge Markers  
![6029d688780756a0d0442751ace62ac49976f8ea815971953965ccd0e66b84ce.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6029d688780756a0d0442751ace62ac49976f8ea815971953965ccd0e66b84ce.jpg)  
See Table 3-1 for taxiway/taxi route width.  
Taxiway Marker Spacing: 15 ft (4.6 m) on straight segments.  
Taxiway Marker Spacing: 10 ft (3.0 m) on curved segments.  
Taxiway Marker Detail: 12-inch (0.3 m) minimum diameter disc at grade or not to exceed 3 inches (76 mm).  
Taxiway Marker Detail: 4-inch (102 mm) diameter × 8-inch (203 mm) high maximum cylinder on a 2-inch (51 mm) support.  
See AC 150/5345-39 for L-853 elevated retroreflective edge markers.

Figure 3-3. Taxiway/Taxi Route Relationship – Unpaved Taxiway with In-Pavement Retroreflective Edge Markers  
![4b627bacbbf3494dcec68dbc570574c90ac26e35f40f0714842b980cad0083f0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4b627bacbbf3494dcec68dbc570574c90ac26e35f40f0714842b980cad0083f0.jpg)  
Taxiway in-pavement retroreflective edge markers 5 ft × 1 ft (1.5 m × 0.3 m).  
Retroreflective edge marker spacing: 15 ft (4.6 m) on straight segments, 10 ft (3 m) on curved segments.  
See Table 3-1 for taxiway/taxi route width.

Table 3-1. Taxiway/Taxi Route Dimensions – GENERAL AVIATION, TRANSPORT, and HOSPITAL Heliports
<table><tr><td rowspan=1 colspan=1>Taxiway(TW)Type</td><td rowspan=1 colspan=1>MinimumWidth ofPaved Area</td><td rowspan=1 colspan=1>CenterlineMarkingType</td><td rowspan=1 colspan=1>TW EdgeMarkingType</td><td rowspan=1 colspan=1>Lateral Separation Between TWEdge Markings</td><td rowspan=1 colspan=1>Total TaxiRouteWidth</td></tr><tr><td rowspan=4 colspan=1>GroundTaxiway</td><td rowspan=2 colspan=1>2 ×UCW</td><td rowspan=2 colspan=1>Painted</td><td rowspan=1 colspan=1>Painted</td><td rowspan=1 colspan=1>2 ×UCW</td><td rowspan=4 colspan=1>1.25D</td></tr><tr><td rowspan=1 colspan=1>Elevated</td><td rowspan=1 colspan=1>0.83 D but not greater than 35 ft(10.7m)</td></tr><tr><td rowspan=2 colspan=1>Unpaved butstabilized for|iground taxi</td><td rowspan=2 colspan=1>None</td><td rowspan=1 colspan=1>In-pavementi</td><td rowspan=1 colspan=1>2×UCW</td></tr><tr><td rowspan=1 colspan=1>Elevated</td><td rowspan=1 colspan=1>0.83 D but not greater than 35 ft(10.7 m)</td></tr><tr><td rowspan=2 colspan=1>HoverTaxiway</td><td rowspan=1 colspan=1>2×UCW</td><td rowspan=1 colspan=1>Painted</td><td rowspan=1 colspan=1>Painted</td><td rowspan=1 colspan=1>2×UCW</td><td rowspan=2 colspan=1>1.67D</td></tr><tr><td rowspan=1 colspan=1>|Unpaved</td><td rowspan=1 colspan=1>None</td><td rowspan=1 colspan=1>Elevated orIn-pavement|id</td><td rowspan=1 colspan=1>0.83 D but not greater than 35 ft(10.7m)</td></tr><tr><td rowspan=1 colspan=6>D      Controlling dimension of the design helicopterTW   TaxiwayUCW Undercarriage Width of the design helicopter</td></tr></table>

Figure 3-4. Hover Taxi Area  
![294ccdcc6b5834d4b9f98ef107e3d2fc53b7495985b22356922a3cddded6932c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/294ccdcc6b5834d4b9f98ef107e3d2fc53b7495985b22356922a3cddded6932c.jpg)  
See paragraph 2.7 for guidance on a TLOF located outside of the FATO.  
Configuration shown recommended by the International Federation of Helicopter Associations.

## 3.4 Taxiway Surfaces.

Guidelines for taxiway surfaces include:

1. For ground taxiways at TRANSPORT heliports, provide a Portland cement concrete or asphalt surface.

2. For ground taxiways at GENERAL AVIATION or HOSPITAL heliports, provide a Portland cement concrete, asphalt, or stabilized surface, such as turf, under the standards of Item P-217 of AC 150/5370-10.

3. For unpaved portions of taxiways and taxi routes, provide a turf cover or treat the surface in some way to prevent dirt and debris from being dispersed by a taxiing helicopter’s rotor down wash.

## 3.5 Taxiway and Taxi Route Gradients.

Design taxiway longitudinal gradients to not exceed 2 percent. Design transverse gradients to be between 0.5 percent and 2 percent.

## 3.6 Helicopter Parking.

If more than one helicopter at a time is expected at a heliport, design the facility with an area specifically designated for parking multiple helicopters. The size of this area depends on the number and size of specific helicopters to be accommodated.

It is not necessary that every parking position accommodate the design helicopter. Design the individual parking positions to accommodate the helicopter sizes and weights expected to use the parking position at the facility. However, use the design helicopter to determine the separation between parking positions and taxi routes. Use the largest helicopter to determine the separation between parking positions intended for helicopters of different sizes. Figure 3-5, Figure 3-6, and Figure 3-7 show typical helicopter parking layouts.

Design helicopter parking per the following guidelines:

1. Design the parking positions to support the static loads of the helicopter intended to use the parking area.

2. Design parking areas as one large, paved, apron or as individual, paved, parking positions.

3. Ground taxi turns of wheeled helicopters are significantly larger than a hover turn. Consider the turn radius of helicopters when designing taxi intersections and parking positions for wheeled helicopters.

4. Design heliport parking areas so helicopters will be parked in an orientation that keeps the “avoid areas” around the tail rotors clear of passenger walkways.

5. A TRANSPORT heliport may have paved areas for helicopter parking and separate paved areas for specific functions such as passenger boarding, maintenance, and parking of based and transient helicopters.

6. Design taxiway longitudinal gradients to not exceed 2 percent. Design transverse gradients to be between 0.5 percent and 2 percent.

Figure 3-5. Typical Parking Area Design – “Taxi-through” Parking Positions.  
![0b99146795ea994043fba7f812f75f0d9d508e1b29710affecdd9d68202d1b78.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0b99146795ea994043fba7f812f75f0d9d508e1b29710affecdd9d68202d1b78.jpg)  
See Chapter 4 for guidance on heliport markings.  
Design the parking positions so that the helicopters exit taxiing forward.  
Minimum clearance between the arcs generated by the main rotor are:  
a. for hover taxi operations, 0.28 D of the larger helicopter, but not less than 10 ft (3 m) b. for ground taxi operations, 10 ft (3 m)  
For paved taxiways and parking positions, the taxiway centerline leads directly into the parking position centerline  
See Table 3-1 for taxiway/taxi route width.

Figure 3-6. Typical Parking Area Design – “Turn-around” Parking Positions  
![f7e0a1673ca97a49bedd4060c8cfcae7f42c10919b1033a612530456da07f4a0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f7e0a1673ca97a49bedd4060c8cfcae7f42c10919b1033a612530456da07f4a0.jpg)  
See Chapter 4 for guidance on heliport markings.  
Minimum clearance between the tail rotor arcs generated by the main rotor arcs are: a. for hover taxi operations, 0.28 D of the larger helicopter, but not less than 10 ft (3 m) b. for ground taxi operations, 10 ft (3 m).  
For paved taxiways and parking positions, the taxiway centerline leads directly into the parking position centerline.  
See Table 3-1 for taxiway/taxi route width.

Figure 3-7. Typical Parking Area Design – “Back-out” Parking Positions  
![8e454765066eb5dfde413c0f27428a894e5e924fcdee18f2c123a3dd0ce03265.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8e454765066eb5dfde413c0f27428a894e5e924fcdee18f2c123a3dd0ce03265.jpg)  
See Chapter 4 for guidance on heliport markings.  
Minimum clearance between the tail rotor arcs generated by the main rotor arcs are:  
a. for hover taxi operations, 0.28 D of the larger helicopter, but not less than 10 ft (3 m)  
b. for ground taxi operations, 10 ft (3 m).  
For paved taxiways and parking positions, the taxiway centerline leads directly into the parking position centerline.  
See Table 3-1 for taxiway/taxi route width.

## 3.6.1 Location.

Guidelines for the location and clearances for helicopter parking include:

1. Locating aircraft parking areas outside of approach/departure surfaces. However, as an option, allow aircraft parking areas under the transitional surfaces.

2. Locating the parking position to provide a minimum distance between the tail rotor arc and any object, building, safety area, or other parking position for “turn-around” parking positions. This minimum distance is 10 feet (3 m) for ground taxi operations and the greater of 10 feet (3 m) or 0.28 D for hover taxi operations. See Figure 3-8.

3. Locating the parking position to provide a minimum distance between the main rotor circle and any object, building, safety area, or other parking position for “taxithrough” and “back-out” parking positions. The minimum distance is 10 feet (3 m) for ground taxi operations and the greater of 10 feet (3 m) or 0.28 D for hover taxi operations. See Figure 3-9.

Locating the parking position to provide a minimum distance between the main rotor circle and the edge of any taxi route. Design parking positions such that the helicopter taxis through, turns around, or backs out to depart. The minimum distance is 0.28 D for “taxi-through” and “turn-around” parking areas, and 0.42 D for “back-out” parking areas. See Figure 3-5, Figure 3-6, and Figure 3-7.

For TRANSPORT heliports, follow these additional helicopter parking guidelines:

a. Locate the parking position to provide a minimum distance between the tail rotor arc and the edge of any taxi route. The standard for this distance is 0.42 D but not less than 30 feet (9.1 m).

b. Do not design “back-out” parking positions at TRANSPORT heliports.

When possible, orient markings such that a pilot would be able to see incoming traffic from the parking position.

Figure 3-8. “Turn-around” Parking Position Marking  
![820d7d5df2c976be32423d90d25d43b9ce603e0dca89c7ce6edab52ae5ff0f9d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/820d7d5df2c976be32423d90d25d43b9ce603e0dca89c7ce6edab52ae5ff0f9d.jpg)  
Base the design of these parking positions on the understanding that the helicopter may pivot about the mast prior to exiting the parking position.  
This marking scheme is for paved areas only. For unpaved parking areas, all that is required is the 0.83 D marking.  
Minimum clearance between the arcs generated by the main rotor arcs and fixed obstacles are: a. for hover taxi operations, 0.28 D of the larger helicopter, but not less than 10 ft (3 m) b. for ground taxi operations, 10 ft (3 m)  
Minimum distance between tail rotor arcs is 0.28 D. If parking areas are different sizes, minimum distance is 0.28 D of the larger design helicopter.  
See Chapter 4 for guidance on heliport markings.

Figure 3-9. “Taxi-through” and “Back-out” Parking Position Marking  
![959cf06a0ddbe29cfc11c777c083d6b227549b464e51be4831382081c3bc7c01.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/959cf06a0ddbe29cfc11c777c083d6b227549b464e51be4831382081c3bc7c01.jpg)  
This marking scheme is for paved areas only. For unpaved parking areas, all that is required is the 0.83 D marking.  
Minimum clearance between 0.83 D parking circle and fixed objects is:  
a. for hover taxi operations, 0.28 D, but not less than 10 ft (3 m)  
b. for ground taxi operations, 10 ft (3 m).  
Minimum distance between 0.83 D parking circle is 0.28 D. If parking areas are different sizes, minimum distance is 0.28 D of the larger design helicopter.  
See Chapter 4 for guidance on heliport markings.

## 3.7 Parking Position Sizes.

3.7.1 Parking position sizes are dependent upon the helicopter size. The clearance needed between parking positions is dependent upon the type of taxi operations (ground taxi or hover taxi) and the intended paths for maneuvering in and out of the parking position. The more demanding requirement will dictate what space is needed at a particular site.

3.7.2 The parking area requirements for skid-equipped helicopters will be the most demanding. The parking requirements for wheeled helicopters may be the most demanding when the largest helicopter is a very large, wheeled aircraft (for example, the S-61), and the skid-equipped helicopters are all much smaller. Design parking areas based on hover taxi operations rather than ground taxi operations if wheel-equipped helicopters taxi with wheels not touching the surface.

3.7.3 Guidelines for parking position size and layout include:

If all parking positions are the same size, design them to accommodate the largest helicopter that will park at the heliport.

“Taxi-through” parking positions are illustrated in Figure 3-5. When using this design exclusively for parking positions, the heliport owner and operator should inform users that “turn-around” departures from the parking position are not permitted.

“Turn-around” parking positions are illustrated in Figure 3-6 and apply to all heliport types.

“Back-out” parking positions can be used for GENERAL AVIATION and HOSPITAL heliports and are illustrated in Figure 3-7. When using this design for parking positions, design the adjacent taxiway to accommodate hover taxi operations so the width of the taxiway will be adequate to support “back-out” operations. (“Back-out” parking positions are not used at TRANSPORT heliports.)

When partially paving a parking area at GENERAL AVIATION or HOSPITAL heliports, design the smallest dimension of the paved parking pad to be a minimum of twice the maximum dimension (length or width, whichever is greater) of the undercarriage or the controlling dimension D, whichever is less, of the largest helicopter that will use the parking position. Place the parking pad in the center of the parking position circle.

When there is more than one parking position, as an option, design the facility with parking positions of various sizes with at least one position that will accommodate the largest helicopter that will park at the heliport. Design other parking positions to be smaller, for the size of the individual or range of individual helicopters parking at that position. Figure 3-10 and Figure 3-11 provides guidance on parking position identification, size, and weight limitations for “turn-around” and “taxi through and backout” parking positions, respectively.

Figure 3-10. Parking Position Identification, Size, and Weight Limitations – Paved Areas, Turn-Around Parking  
![e8039efb23684d99450c5e051fea9e0c1a438b566d854550790747d3e3a8607d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/e8039efb23684d99450c5e051fea9e0c1a438b566d854550790747d3e3a8607d.jpg)  
This marking scheme is for paved areas only. For unpaved parking areas, all that is required is the 0.83 D marking, with optional TDPC marking.  
See Chapter 4 for guidance on heliport markings.

Figure 3-11. Parking Position Identification, Size, and Weight Limitations – Paved Areas, “Taxi-through” and “Back-out” Parking  
![ac54b388c7ce4e94a49be602795e9d33550ef9a0e6dfbac8aef39f6247b57029.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ac54b388c7ce4e94a49be602795e9d33550ef9a0e6dfbac8aef39f6247b57029.jpg)  
This marking scheme is for paved areas only. For unpaved parking areas, all that is required is the 0.83 D, with optional TDPC marking.  
See Chapter 4 for guidance on heliport markings.

## 3.8 Walkways.

At helicopter parking positions, provide marked ingress/egress walkways where practicable.

Design the pavement to drain away from walkways so spilled fuel does not drain onto walkways or toward parked helicopters.

Locate passenger walkways to minimize passenger exposure to various risks during passenger loading and unloading.

For TRANSPORT heliports, provide marked ingress/egress walkways.

## 3.9 Fueling.

Design the heliport facility to allow fueling with the use of a fuel truck or a specific fueling area with stationary fuel tanks. Guidelines for design of the fueling area include:

For ground-based heliports, do not locate fueling equipment in the TLOF or FATO.

Do not locate fueling equipment directly under the approach/departure surfaces.

Low profile fueling equipment can be located in the safety area if there is not available room outside the safety area. Low profile fuel dispensing cabinets can be located in one quadrant of a safety area if they are marked and lighted, and the other three quadrants of the safety area are clear. Do not locate the dispensing cabinet directly under approach/departure surfaces.

Design and mark fueling facilities to minimize the potential for helicopters to collide with the dispensing equipment.

Design fueling areas so there is no object tall enough to be hit by the main or tail rotor blades within a distance of D of the design helicopter from the center point of the position where the helicopter would be fueled (providing a minimum of 0.42 D clearance from the rotor tips). If this is not practical at an existing facility, install long fuel hoses.

Provide area lighting of the fueling area if night fueling operations are contemplated. Ensure any light poles do not constitute an obstruction hazard.

Various federal, state, and local requirements for petroleum handling facilities apply to systems for storing and dispensing fuel. Guidance is provided in AC 150/5230-4, Aircraft Fuel Storage, Handling, and Dispensing on Airports. Additional information may be found in various National Fire Protection Association (NFPA) publications. For additional reference material, see Appendix E.

## 3.10 Tiedowns.

Install recessed tiedowns to accommodate extended or overnight parking of based or transient helicopters.

Recess any tiedowns so they will not be a hazard to helicopters or a trip hazard for personnel. As an option, highlight each tiedown point with a bright contrasting color of paint for pedestrian safety.

Ensure any depression associated with the tiedowns is of a diameter not greater than half the width of the smallest helicopter landing wheel anticipated to be operated on the heliport surface. In addition, provide storage for tiedown chocks, chains, cables, and ropes off the heliport surface to avoid fouling landing gear.

Guidance on recessed tiedowns is provided in AC 20-35, Tiedown Sense.

# Page Intentionally Blank

## CHAPTER 4. Heliport Markings and Lighting

## 4.1 General.

This chapter provides guidance on heliport markings and lighting for all three types of heliports and for paved and non-paved surfaces.

## 4.2 Heliport Retroreflective Markers and Markings.

Markers and/or surface markings identify the facility as a heliport per the following guidelines.

Use paint or preformed materials for surface markings. (See AC 150/5370-10, Item P-620, Runway and Taxiway Marking, for specifications for paint and preformed material.).

As an option, use reflective paint and retroreflective markers, though overuse of reflective material can be blinding to a pilot using landing lights and/or night vision goggles.

As an option, outline lines/markings with a 6-inch (152 mm) wide line of a contrasting color to enhance conspicuity.

Place markings that define the edges of a TLOF, FATO, taxiway, or apron within the limits of those areas.

As an option, use the retroreflective markers and markings, as described in paragraph 4.3 through paragraph 4.12.

Overuse of reflective materials can cause glare to a pilot using landing lights and/or night vision goggles.

## 4.3 Standard Heliport Identification Marking.

The heliport identification marking (or symbol) identifies the location as a heliport, marks the TLOF, and provides visual cues to the pilot. See Figure 4-1 and Figure 4-2 for dimensional standards for these markings. Guidelines for this marking include:

Locate the “H” in the center of the TLOF and orient it on the axis of the primary or preferred approach/departure path.

Place a one-foot-wide bar under the “H” when it is necessary to distinguish the preferred approach/departure direction. See Figure 4-1.

## 4.3.1 PPR Heliport Optional (Nonstandard) Heliport Identification Marking.

For a PPR heliport, consider the following:

An optional distinctive marking can be used, such as a company logo, to identify the facility as a PPR heliport.

A nonstandard marking does not necessarily provide the pilot with the same degree of visual cueing as the standard heliport identification symbol.

To compensate for potential decreased visual cueing, increase the size of the safety area to the extent practical when the standard heliport identification symbol “H” is not used.

## 4.3.2 HOSPITAL Heliports Alternative Identification Marking.

As an alternative to the standard marking for HOSPITAL heliports, use a red “H” with a white 6-inch (152 mm) wide border within a red cross with a 12-inch (0.3 m) wide white border and a surrounding red TLOF.

Where it is impractical to paint the whole TLOF red, paint the TLOF so the minimum dimension (length, width, or diameter) of the outer red area is equal to 0.83 D of the design helicopter but not less than 40 feet (12.2 m). Figure 4-4 illustrates this alternative marking.

## 4.3.3 Private-use (PVT) Identification Marking.

An optional “PVT” marking may be used to indicate a private-use heliport. Text height is a minimum of 3 feet (0.9 m). The preferred maximum height is 5 feet (1.5 m).

## 4.3.4 HOSPITAL Heliport: Marking for Winter Operations.

In winter weather at a heliport with a dark TLOF surface, the marking shown in Figure 4-4 will absorb more heat from the sun, may reduce glare, and more readily melt residual ice and snow. In contrast, the white area in Figure 4-3 is more likely to be icy during winter weather. Consequently, in areas that experience ice and snow, use the markings in Figure 4-4 for unheated TLOFs.

Figure 4-1. Standard TLOF Markings  
![6d266cb91beaefdf09261a8638f5c2e1dd7755e8af12ce8479340531cf09e8c4.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6d266cb91beaefdf09261a8638f5c2e1dd7755e8af12ce8479340531cf09e8c4.jpg)

![99468ef8eb4c45702f48d87a0d77216bd729c9eabf8826b3cb61a3a6f41afa58.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/99468ef8eb4c45702f48d87a0d77216bd729c9eabf8826b3cb61a3a6f41afa58.jpg)  
For GENERAL AVIATION and TRANSPORT heliports, mark the TLOF with a white “H” marking (see Figure 4-3). For HOSPITAL heliports, see Figure 4-2, Detail A, for dimensions.  
Place a 1-foot black bar 2 feet (0.6 m) below the “H” marking when it is necessary to distinguish the preferred approach/departure direction.  
See Figure 4-2, Detail B, for dimensions.

Figure 4-2. Standard Heliport Identification Symbol, TLOF Size and Weight Limitations  
![54a617f0a059dd785976e84d97436c515ae16358acfee8e3c220a8c5c5148830.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/54a617f0a059dd785976e84d97436c515ae16358acfee8e3c220a8c5c5148830.jpg)

<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=2>“H&quot;Size</td></tr><tr><td rowspan=1 colspan=1>Dimension</td><td rowspan=1 colspan=1>StandardTLOF marking</td><td rowspan=1 colspan=1>AlternateTLOF marking</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>10-0&quot;[3 m]</td><td rowspan=1 colspan=1>0.3D</td></tr><tr><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>6-8&quot;[2 m]</td><td rowspan=1 colspan=1>0.66A</td></tr><tr><td rowspan=1 colspan=1>C</td><td rowspan=1 colspan=1>1-0&quot;[0.3 m]</td><td rowspan=1 colspan=1>0.1A</td></tr><tr><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>0^-3&quot;[76 mm]</td><td rowspan=1 colspan=1>0.02A</td></tr><tr><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>2-0&quot;[0.6 m]</td><td rowspan=1 colspan=1>0.2A</td></tr></table>

Detail A Heliport identification symbol

![f4583570997198e527c33aa6930febb66cb430c7e7e471eb66b3e4945def9f0b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f4583570997198e527c33aa6930febb66cb430c7e7e471eb66b3e4945def9f0b.jpg)  
No weight limit

![b05f6dbdaa85701b30996b9f9c65d71f775a285a1c8f2059ba3d7b7d9e0180c2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/b05f6dbdaa85701b30996b9f9c65d71f775a285a1c8f2059ba3d7b7d9e0180c2.jpg)  
Alternate marking with no weight restrictions

Detail B TLOF size/weight limitation box

See Appendix D for the form and proportion of the numbers used in the TLOF Size and Weight Limitation Box.

Make the minimum size of the box 5 ft (1.5 m) square. Where possible, increase this dimension to a 10 ft (3 m) square for improved visibility.

Characters within the TLOF Size and Weight Limitation Box are black on a white background.

“4” indicates the maximum takeoff weight (4,000 lbs (1,814 kg)) of the TLOF design helicopter, in units of thousands of pounds.

“D40” indicates the controlling dimension D of the largest helicopter (40 ft (12.2 m)) for which the TLOF is designed.

See paragraph 4.4.3 for application of size/weight limitation box.

For GENERAL AVIATION and TRANSPORT heliports, mark the TLOF with a white “H” marking. For HOSPITAL heliports, mark the TLOF with a red “H” in a white cross.

Figure 4-3. HOSPITAL Heliport – Standard Identification Marking  
![58e9cf21d3666cae2721bd7f85a800db4bf122c426111f44b4d6e8091fc9fee3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/58e9cf21d3666cae2721bd7f85a800db4bf122c426111f44b4d6e8091fc9fee3.jpg)  
Standard TLOF perimeter strip of 12 inches (0.3 m) wide. See Figure 4-2 for “H”, touchdown position, controlling dimension D, and weight limitation box dimensions.

Figure 4-4. HOSPITAL Heliport – Alternative Identification Marking  
![8a72f06427df07477498979be84b6112ad98357b3eb802ed8aa634d14f41ebbc.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8a72f06427df07477498979be84b6112ad98357b3eb802ed8aa634d14f41ebbc.jpg)  
Standard TLOF perimeter strip of 12 inches (0.3 m) wide. See Figure 4-2 for “H”, touchdown position, controlling dimension D, and weight limitation box dimensions.

## 4.4 TLOF and FATO Markings.

## 4.4.1 TLOF and Optional FATO Perimeter Retroreflective Markings.

Define the TLOF perimeter with retroreflective markers and/or lines as follows:

If the heliport operator does not mark the TLOF, increase the size of the safety area, as described in paragraph 2.9.

See Figure 4-5 for perimeter markings for TRANSPORT heliports and other paved or hard surfaced TLOFs.

See Figure 4-6 for perimeter markings for unpaved TLOFs at GENERAL AVIATION or HOSPITAL heliports.

Figure 4-5. Paved TLOF/Paved FATO – Paved TLOF/Unpaved FATO – Marking: TRANSPORT Heliports and Other Heliports with a Paved TLOF  
![2d8107429c479b6f5f653d81893e451b061a1b4e47dd0e306e35492e4a1495f9.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2d8107429c479b6f5f653d81893e451b061a1b4e47dd0e306e35492e4a1495f9.jpg)  
Mark the perimeter of the TLOF and FATO.

Define the perimeter of a paved or hard surfaced TLOF with a continuous 12 inch (0.3 m) white line.

Define paved load-bearing FATO perimeters with a 12 inch (0.3 cm) wide dashed line per Detail A.

Define unpaved load-bearing FATO perimeters with in-pavement retroreflective markers per Detail A.

See Figure 4-2 for “H”, touchdown/position, controlling dimension D, and weight box dimensions.

Figure 4-6. Unpaved TLOF/Unpaved FATO – Marking: GENERAL AVIATION and HOSPITAL Heliports  
![d4958598ccba0b9c573d9fc0d004e5bd6d502de5578e88332cf54325ac083564.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d4958598ccba0b9c573d9fc0d004e5bd6d502de5578e88332cf54325ac083564.jpg)  
Mark the perimeter of the TLOF.  
FATO markings are optional if the TLOF is marked but are included if the TLOF is not marked.  
Define an unpaved load-bearing TLOF perimeter with in-pavement retroreflective markers per Detail A.  
Define an unpaved load-bearing FATO perimeter with in-pavement retroreflective markers per Detail B.  
See Figure 4-2 for “H”, touchdown/position, controlling dimension D, and weight limitation box dimensions.

## 4.4.2 Touchdown/Positioning Circle (TDPC) Marking.

A TDPC marking provides guidance to allow a pilot to touch down in a specific position within the TLOF. This marking is intended to ensure the pilot’s seat is over the marking, the undercarriage will be inside the LBA, and all parts of the helicopter will be clear of any obstacle by a safe margin.

A TDPC marking is a yellow circle with an inner diameter of 1/2 D and a line width of 18 inches (0.5 m). Locate a TDPC marking in the center of a TLOF. See Figure 4-6.

At PPR heliports, the TDPC marking may be omitted as an option where the TLOF width is less than 16 feet (4.9 m).

## 4.4.3 TLOF Size and Weight Limitations Markings.

Install size and weight limitations per the following guidelines:

Mark the TLOF to indicate the controlling dimension D and weight of the largest helicopter that the heliport will accommodate, as shown in Figure 4-2.

Place these markings in a box in the lower right-hand corner of a rectangular TLOF, or on the right-hand side of the “H” of a circular TLOF, when viewed from the preferred approach direction.

If necessary, allow the size and weight limitation box marking to interrupt the TDPC marking.

The numbers are black with a white background. See Appendix D for details on the form and proportions of the numbers and letters specified for these markings.

Do not use metric equivalents for this purpose.

These size and weight limitations markings are optional for a TLOF with a turf surface.

These size and weight limitation markings are optional for PPR heliports, since the operator ensures that all pilots using the PPR facility are thoroughly knowledgeable with this and any other facility limitations.

## 4.4.3.1 TLOF Size Limitation.

This number is the controlling dimension D of the largest helicopter the TLOF will accommodate, as shown in Figure 4-2.

The marking consists of the letter “D” followed by the dimension in feet.

Center this marking in the lower section of the TLOF size/weight limitation box.

## 4.4.3.2 TLOF Weight Limitations.

If a TLOF has limited weight-carrying capability, mark it with the maximum takeoff weight of the design helicopter, in units of thousands of pounds, as shown in Figure 4-2.

Center this marking in the upper section of a TLOF size/weight limitation box.

For ground-based facilities with no weight limit, add a diagonal line, extending from the lower left-hand corner to the upper right-hand corner, to the upper section of the TLOF size/weight limitation box, as illustrated in Detail B of Figure 4-2.

## 4.5 Extended Pavement/Structure Markings for GENERAL AVIATION and HOSPITAL Heliports.

As an option, increase the area of the pavement or structure without a corresponding increase in the length and width, or diameter of the FATO, to accommodate pedestrians and/or support operations. Whether or not this increased area is part of the LBA, mark the pavement or area outside the TLOF with 12-inch-wide (0.3 m) diagonal black and white stripes. See Figure 4-7 for marking details.

## 4.6 FATO Perimeter Markings.

Define the perimeter of a load-bearing FATO with retroreflective markers and/or lines. Do not mark the FATO perimeter if any portion of the FATO is not a load-bearing surface. In such cases, mark the perimeter of the LBA, as described below.

## 4.6.1 Paved FATOs.

Define the perimeter of a paved load-bearing FATO with a 12-inch-wide (0.3 m) dashed white line. Clearly define the corners of the FATO with these white perimeter markings. The perimeter marking segments are approximately 5 feet (1.5 m) in length, and with end-to-end spacing of approximately 5 feet (1.5 m). See Figure 4-5.

## 4.6.2 Unpaved FATOs.

Define the perimeter of an unpaved load-bearing FATO with 12-inch-wide (0.3 m) inground retroreflective markers. Clearly define the corners of the FATO with perimeter retroreflective markers. The rest of the perimeter retroreflective markers are 5 feet (1.5 m) long, and have end-to-end spacing of approximately 5 feet (1.5 m). See Figure 4-6.

Figure 4-7. Extended Pavement/Structure Marking: GENERAL AVIATION and HOSPITAL Heliports

# Extended pavement structure TLOF edge marki

Extended pavement/structure markings begin in-pavement with TLOF edge markings, and end at the edge, of the extended pavement/structure.

Extended pavement/structure markings are 12 inches (0.3 m) wide black and white stripes on a 45° angle.

## 4.7 Flight Path Alignment Guidance Marking.

An optional flight path alignment guidance marking consists of one or more arrows to indicate the preferred approach/departure direction(s). Place the guidance marking on the TLOF, FATO, and/or safety area surface, as shown in Figure 2-19.

When combined with a flight path alignment guidance lighting system, described in paragraph 2.12.4, it takes the form shown in Figure 2-19, which includes scheme for marking and lighting the arrows.

The shaft of each arrow is 18 inches (0.5 m) in width and recommended length is 10 feet (3 m).

Use a color which provides good contrast against the background color of the surface.

An arrow pointing toward the center of the TLOF depicts an approach direction.

An arrow pointing away from the center of the TLOF depicts a departure direction.

In the case of a flight path limited to a single approach direction or a single departure path, the arrow marking is unidirectional (e.g., one arrowhead only). In the case of a heliport with only a bidirectional approach/takeoff flight path available, the arrow marking is bidirectional (e.g., two arrowheads).

## 4.8 Taxiway and Taxi Route Markings.

## 4.8.1 Paved Taxiway Markings.

For all heliports, mark the centerline of a paved taxiway with a continuous 6-inch (152 mm) yellow line, For TRANSPORT heliports, mark both edges of the taxiway with two continuous 6-inch (152 mm) wide yellow lines spaced 6 inches (152 mm) apart. For GENERAL AVIATION and HOSPITAL heliports, provide optional taxiway edge markings to increase conspicuity. Figure 3-1 illustrates taxiway centerline and edge markings.

## 4.8.2 Unpaved Taxiway Markings.

Where taxiways are not paved, install either elevated or in-pavement retroreflective edge markers to provide strong visual cues to pilots at both GENERAL AVIATION and HOSPITAL heliports.

Space retroreflective markers longitudinally at approximately 15-foot (4.6 m) intervals on straight segments and at approximately 10-foot (3 m) intervals on curved segments.

Figure 3-2 and Figure 3-3 illustrate these taxiway edge markings/retroreflective markers.

Elevated retroreflective edge markers are blue, 4 inches (102 mm) diameter × 8 inches (203 mm) high maximum cylinder on a 2-inch (51 mm) support.

In-pavement retroreflective edge markers are yellow, 12 inches (0.3 m) wide, and approximately 5 feet (1.5 m) long.

## 4.8.3 Elevated Retroreflective Edge Markers in Grassy Areas.

Tall grass sometimes obscures elevated retroreflective edge markers. Address this issue by installing 12-inch (0.3 m) diameter solid-material disks around the poles supporting the elevated retroreflective markers. Ensure grass and other vegetation is cut short or removed from around these edge markers to a minimum radius of 2 feet (0.6 m).

## 4.8.4 Taxiway to Parking Position Transition Requirements.

For paved taxiways and parking areas, taxiway centerline markings continue into parking positions and become the parking position centerlines.

## 4.9 Helicopter Parking Position Markings.

Helicopter parking positions have the following markings.

## 4.9.1 Paved Parking Position Identifications.

Mark parking position identifications (numbers or letters) if there is more than one parking position. These markings are yellow characters 36 inches (0.9 m) high. See Figure 3-10 and Figure D-1.

## 4.9.2 Parking Circle.

Define the circle of radius 0.83 D of the largest helicopter that will park at that position with a 6-inch (152 mm) wide, solid yellow line with an outside diameter of 0.83 D.

In paved areas, this is a painted line (see Figure 3-8 and Figure 3-9).

In unpaved areas, use a series of in-pavement retroreflective markers, 6 inches (152 mm) in width, a maximum of 5 feet (1.5 m) in length, and with end-to-end spacing of approximately 5 feet (1.5 m).

## 4.9.3 Touchdown/Positioning Circle (TDPC) Marking.

An optional TDPC marking provides guidance to allow a pilot to touch down in a specific position on paved surfaces. When the pilot’s seat is over the marking, the undercarriage will be inside the LBA, and all parts of the helicopter will be clear of any obstacle by a safe margin.

A TDPC marking is a yellow circle with an inner diameter of 1/2 D and a line width of 18 inches (0.5 m).

Locate a TDPC marking in the center of a parking position. See Figure 3-8.

The FAA recommends a TDPC marking for “turn-around” parking areas.

## 4.9.4 Maximum Length Marking.

This marking on paved surfaces indicates the D of the largest helicopter that the position is designed to accommodate (for example, 49). This marking consists of yellow characters at least 36 inches (0.9 m) high. See Figure 3-10 and Appendix D.

## 4.9.5 Parking Position Weight Limit.

If a paved parking position has a weight limitation, mark it in units of 1,000 lbs (454 kg), as illustrated in Figure 3-10. (For example, a “4” indicates a weight-carrying capability of up to 4,000 lbs (1,814 kg) a “12” up to 12,000 lbs (5,443 kg).)

Do not use metric equivalents for this purpose.

This marking consists of yellow characters 36 inches (0.9 m) high.

When necessary to minimize the possibility of being misread, place a bar under the number.

See Figure 3-10 and Appendix D for additional parking position weight limit information.

## 4.9.6 Pavement Shoulder Markings.

As an option, use pavement shoulder markings for paved parking areas (Figure 3-9) to ensure safe rotor clearance.

Install a 6-inch (152 mm) wide solid yellow shoulder line, perpendicular to the centerline and extending to the 0.83 D marking, so it is under the pilot’s shoulder such that the main rotor of the largest helicopter the position will accommodate will be entirely within the rotor diameter parking circle (see Figure 3-9).

Use 1/4 D from the center of the parking area to define the location of shoulder line.

The FAA recommends a shoulder line marking for both “taxi-through” and “backout” parking areas.

## 4.10 Walkways.

Figure 3-10 illustrates one marking scheme for walkways.

## 4.11 Closed Heliport.

Remove all markings of a permanently closed heliport, FATO, or TLOF. If it is impractical to remove the markings, place a yellow “X” over the $\mathbf { \bar { \Sigma } } ^ { \mathsf { e } } \mathbf { \Psi } \mathbf { H } ^ { \mathsf { p } } )$ , as illustrated in Figure 4-8.

For temporary heliport closures, as an option, place a yellow “X” over the “H”. See Figure 4-8.

Make the yellow “X” large enough to ensure early pilot recognition that the heliport is closed.

Remove the wind cone(s) and other visual indications of a closed heliport.

Turn off and disconnect heliport perimeter lighting and other lighting for the heliport.

Figure 4-8. Marking a Closed Heliport  
![7a26517c047a47891424d6c5b0e91fa4165ab74ee95fa7c32cbc03272bced265.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7a26517c047a47891424d6c5b0e91fa4165ab74ee95fa7c32cbc03272bced265.jpg)  
See paragraph 4.11 for guidance on removal of markings for permanent or temporary heliport closures.

## 4.12 Marking Sizes.

See Appendix D for guidance on the proportions and sizes of painted numbers and letters.

## 4.13 Heliport Lighting.

Heliports that support night operations under visual meteorological conditions or instrument meteorological conditions for either day or night operations are lighted with TLOF and/or optional FATO perimeter lights, as described below. FATO perimeter lights may be used as an option under special circumstances to improve visual acquisition of the approach path and/or landing environment due to varying degrees of ambient light, proximity to airport taxiways, etc.

Install FAA type L-860H elevated and/or FAA type L-852H in-pavement light fixtures for heliport perimeter applications for VMC applications.

Light intensity and horizontal/vertical light distribution are characterized.

The light emitting diode (LED) elevated heliport fixture and LED in-pavement fixture will be identified as: L-860H (L) and L-852H (L), respectively.

Any of these fixtures may be used as flight path alignment lights or landing direction lights.

See Appendix G for heliport perimeter lighting design requirements.

Ensure elevated navigational aids (NAVAIDS) do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).

## 4.13.1 In-pavement TLOF Perimeter Lights.

Install TLOF perimeter lights, per the guidelines below, as shown in Figure 4-9, Figure 4-10, and Figure 4-11.

Install FAA type L-852H in-pavement green lights meeting the requirements in Appendix G to define the TLOF perimeter.

For heliports where only the TLOF is load-bearing, install FAA type L-852H inpavement green lights or, as an option, install elevated green omnidirectional lights.

Use a minimum of four light fixtures per side of a square or rectangular TLOF. For HOSPITAL and PPR Heliports, as an option, use a minimum of three light fixtures per side of a square or rectangular TLOF.

Use an odd number of lights on each side to place lights along the centerline of the approach.

Locate a light at each corner, with additional lights uniformly spaced between corner lights. Space the lights at a maximum of 25 feet (7.6 m).

For a circular TLOF, use an even number of lights, with a minimum of eight, uniformly spaced.

Locate in-pavement lights within 1 foot (0.3 m) inside or outside of the TLOF perimeter.

Locate elevated lights outside and within 10 feet (3 m) of the edge of the TLOF. Ensure elevated lights do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).

As an option for TLOF lights at TRANSPORT heliports, install a line of 7 green, in-pavement lights meeting the standards in Appendix G. Space these lights at 5- foot (1.5 m) intervals in the TLOF pavement. Align these lights on the centerline of the approach course to provide close-in directional guidance and improve TLOF surface definition. See Figure 4-11.

For PPR heliports, install in-pavement TLOF lights. As an option, if the FATO is load-bearing, use elevated omnidirectional lights. For private-use heliports, install elevated omnidirectional or in-pavement lighting in the TLOF as appropriate to site specific surface materials, elevations, and weather conditions.

Mount perimeter lights on the outer edge of the pavement or structure or the inner edge of the safety net as an option when the pavement or structure is larger than the TLOF.

Figure 4-9. Elevated TLOF – Perimeter Lighting  
![28586bf2a4d0ce20892c4793890522bb6b2524b3ee877aeacd111c2ada932a11.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/28586bf2a4d0ce20892c4793890522bb6b2524b3ee877aeacd111c2ada932a11.jpg)  
Install either “A” Type L-852H, or “B” Type L-860H.  
In-pavement edge light fixture Ⓐ (Type L-852H).  
Omnidirectional light Ⓑ, mounted off the structure edge (Type L-860H).  
Ensure elevated lights do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).  
For TLOF and FATO lighting requirements, see Appendix G.  
A safety net’s supporting structure should be located below the safety net.

Figure 4-10. TLOF/FATO Perimeter Lighting  
![573bbbfbf7d72fb638d9b27b4d3f151d3d741f8371409d97beef89f8e4233c68.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/573bbbfbf7d72fb638d9b27b4d3f151d3d741f8371409d97beef89f8e4233c68.jpg)  
Install in-pavement TLOF perimeter lights inside or outside within 1 ft (0.3 m) of the FATO and TLOF respective perimeters. FATO lighting installation is optional but may be installed for specific applications.  
TLOF/FATO Lighting: 25 ft (7.6 m) maximum spacing, 4 lights per side minimum.  
Approach Lighting: 15 ft (4.6 m) spacing. Elevated FATO omnidirectional lights (optional).  
Install in-pavement edge light fixtures in accordance with the requirements of AC 150/5340-30.  
For TLOF and FATO lighting requirements, see Appendix G.

Figure 4-11. TLOF In-pavement and FATO Elevated Perimeter Lighting  
![0565c4b0b984cc131dbe082280ae00e3f465ea03d823a4a80143b0b9a77e3e84.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0565c4b0b984cc131dbe082280ae00e3f465ea03d823a4a80143b0b9a77e3e84.jpg)  
Install in-pavement FATO and TLOF perimeter lights inside or outside within 1 ft (0.3 m) of the FATO and TLOF respective perimeters.  
Locate a light at each corner with additional lights uniformly spaced between the corner lights with a maximum spacing of 25 feet (7.6 m) between lights.

Install an odd number of edge lights on each side to place lights along the centerline of the approach.

Install elevated FATO lights 10 ft (3 m) outside the FATO perimeter.

TLOF/FATO Lighting: 25 ft (7.6 m) maximum spacing, 4 lights per side minimum.

Position the approach lights with 15 ft (4.6 m) spacing.

Elevated FATO omnidirectional lights. See Appendix G.

Ensure the elevated lights do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).

## 4.13.2 Perimeter Lights for Elevated TLOFs.

As an option for heliports, use elevated, omnidirectional lights meeting the requirements of Appendix G.

Locate these lights on the outside edge of the TLOF.

Ensure the elevated lights do not penetrate a horizontal plane at the TLOF edge elevation by more than 2 inches (51 mm). See Figure 4-9.

## 4.13.3 Optional FATO Perimeter Lights

Design guidelines for optional FATO perimeter lights are provided below for TRANSPORT heliports, GENERAL AVIATION and HOSPITAL heliports as these guidelines are distinct for each type of heliport, as shown in Table 4-1. See also Figure 4-10, Figure 4-11, and Figure 4-12.

When a heliport on an airport is sited near an aircraft taxiway, there may be a concern that a pilot may confuse the green taxiway centerline lights with the FATO perimeter lights. As an option in such cases, use yellow lights as an alternative color for marking the FATO.

Table 4-1. FATO Perimeter Light Design
<table><tr><td colspan="1" rowspan="1"></td><td colspan="1" rowspan="1">TRANSPORT FATO</td><td colspan="1" rowspan="1">GA/HOSPITALLoad-bearing FATO</td></tr><tr><td colspan="1" rowspan="1">Lights</td><td colspan="1" rowspan="1">Use green lights meeting therequirements of Appendix Gto define the limits of theFATO.</td><td colspan="1" rowspan="1">• Use green lights meeting the requirements ofAppendix G to define the perimeter of a load-bearing FATO. Do not light the FATO perimeter if anyportion of the FATO is not a load-bearingsurface.</td></tr><tr><td colspan="1" rowspan="1">Locationand spacing</td><td colspan="1" rowspan="1">• See Figure 4-11 for lightspacing and layout.</td><td colspan="1" rowspan="1"> Install a minimum of four (minimum of threelights for PPR and HOSPITAL heliports) in- pavement per side of a square or rectangularFATO.• Space lighting 25 ft (7.6 m) maximumspacing.</td></tr><tr><td colspan="1" rowspan="1">Installationguidance</td><td colspan="1" rowspan="1">• Mount frangible elevatedlight fixtures 10 feet (3 m) outfrom the FATO perimeter.• Ensure they do not penetrate ahorizontal plane at theadjacent TLOF elevation bymore than 2 inches (51 mm).</td><td colspan="1" rowspan="1">• N/A</td></tr><tr><td colspan="1" rowspan="1">ElevatedFATO</td><td colspan="1" rowspan="1">Lighting for an elevatedFATO is the same as for aground-level FATO.Ensure the elevated lights donot penetrate a horizontalplane at the adjacent TLOF</td><td colspan="1" rowspan="1">• In the case of an elevated FATO with a safetynet, mount the perimeter lights, as described in paragraph 4.13.2.• As an option, locate elevated FATO perimeterlights, no more than 2 inches (51 mm) high,</td></tr><tr><td></td><td>elevation by more than 2 inches (51 mm).</td><td>10 feet (3 m) from the FATO perimeter. See Figure 4-11. Ensure the elevated lights do not penetrate a horizontal plane at the adjacent TLOF elevation by more than 2 inches (51 mm).</td></tr><tr><td>Circular FATO</td><td>• N/A</td><td>To define a circular FATO, use an even number of lights, with a minimum of eight light fixtures uniformly spaced. Locate in-pavement lights within 1 foot (0.3 m) inside or outside of the FATO perimeter See Figure 4-10. As an option, use a square or rectangular pattern of FATO perimeter lights even if the TLOF is circular. At a distance during nighttime operations, a square or rectangular pattern of FATO perimeter lights may provide the pilot with better visual alignment cues than a circular pattern, but a circular pattern may be more effective in an urban environment.</td></tr></table>

Figure 4-12. FATO Elevation  
![d10d29e97c83f9828366878777d1d78cf5c8bf8bc6451ce1b4e01883de709a06.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d10d29e97c83f9828366878777d1d78cf5c8bf8bc6451ce1b4e01883de709a06.jpg)  
See paragraph 4.13.3 for guidance on FATO lights.

## 4.13.4 Floodlights.

The FAA has not evaluated floodlights for effectiveness in visual acquisition of a heliport. Guidelines for the use and installation of floodlights includes:

TRANSPORT Heliports – Install floodlights to illuminate the helicopter parking areas.

GENERAL AVIATION and HOSPITAL Heliports – Install floodlights to illuminate the TLOF, the FATO, and/or the parking area if ambient light does not suitably illuminate markings for night operations.

Mount these floodlights on adjacent buildings to eliminate the need for tall poles, if possible. Place floodlights clear of the TLOF, the FATO, the safety area, the approach/departure surfaces, and transitional surfaces and ensure floodlights and their associated hardware do not constitute an obstruction hazard.

Aim floodlights down to provide adequate illumination on the apron and parking surface.

Ensure floodlights that might interfere with pilot vision during takeoff and landings are capable of being turned off by pilot control or at pilot request.

Note 1: Floodlights do not replace TLOF or FATO lighting recommendations.

Note 2: White lighting for heliport applications should not be activated until the aircraft has landed and deactivated prior to takeoff.

## 4.13.5 Landing Direction Lights.

Install landing direction lights when it is necessary to provide directional guidance to indicate available approach and/or departure path directions as an option, as follows:

Landing direction lights are a configuration of five green, omnidirectional lights meeting the standards of Appendix G, located on the centerline of the preferred approach/departure paths.

Space these lights at 15-foot (4.6 m) intervals extending outward in the direction of the preferred approach/departure paths, with spacing and layout, as illustrated in Figure 4-13.

Figure 4-13. Landing Direction Lights.  
![9eec2cfa58b6e646fc86eb5ccf11d34c20450f0cd1f175a9fa035650b04cbe95.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9eec2cfa58b6e646fc86eb5ccf11d34c20450f0cd1f175a9fa035650b04cbe95.jpg)  
Locate the first omnidirectional landing direction light 20-60 ft (6.1-18.3 m) from the TLOF for GENERAL AVIATION and HOSPITAL heliports, and 30-60 ft (9.1-18.3 m) from the TLOF for TRANSPORT heliports.  
See paragraph 4.13.5 for guidance on landing direction lights.

## 4.13.6 Flight Path Alignment Lights.

Flight path alignment lights provide approach and/or departure path directions in a straight line along the direction of approach and/or departure flight paths. If necessary, they may extend across the TLOF, FATO, safety area, or any suitable surface in the immediate vicinity of the FATO or safety area. Use three or more green lights spaced at 5 ft (1.5 m) to 10 ft (3 m).

Install flight path alignment lights meeting the requirements of Appendix G as an option.

Place these lights in a straight line along the direction of approach and/or departure flight paths.

Extend the lights across the TLOF, FATO, safety area, or any suitable surface in the immediate vicinity of the FATO or safety area, if necessary.

Install three or more green lights spaced at 5 feet (1.5 m) to 10 feet (3 m). See Figure 2-19.

## 4.13.7 Taxiway and Taxi Route Lighting.

## 4.13.7.1 Optional Taxiway and Taxi Route Lighting.

Install taxiway centerline lights per the following guidelines:

Install in-pavement bidirectional green taxiway centerline lights meeting the standards of AC 150/5345-46, Specification for Runway and Taxiway Light Fixtures, for type L-852A (straight segments) or L-852B (curved segments).

Space these lights at maximum 50-foot (15.2 m) longitudinal intervals on straight segments and at maximum 25-foot (7.6 m) intervals on curved segments, using a minimum of four lights to define the curve.

Uniformly offset the taxiway centerline lights no more than two feet (0.6 m) to facilitate painting of the taxiway centerline.

For GENERAL AVIATION and HOSPITAL Heliports, green retroreflective markers can be used as an option in lieu of the L-852A or L-852B lighting fixtures.

Use Type I retroreflective markers, as described in AC 150/5345-39, Specification for L-853, Runway and Taxiway Retroreflective Markers.

Do not use retroreflective markers for TRANSPORT heliports.

## 4.13.7.2 Optional Taxiway Edge Lights.

Specify taxiway edge lights per the following guidelines:

For paved taxiways, use type L-852T in-pavement omnidirectional blue lights meeting the standards of AC 150/5345-46 to mark the edges of a taxiway.

Use type L-861T elevated lights meeting the standards of AC 150/5345-46. The lateral spacing for the lights or reflectors is equal to 0.83 D of the design helicopter, but not more than 35 feet (10.7 m).

For unpaved taxiways at GENERAL AVIATION and HOSPITAL heliports, blue retroreflective markers may be used in lieu of lights.

Ensure retroreflective markers are no more than 8 inches (203 mm) tall.

TRANSPORT heliports cannot use retroreflective markers.

Install taxiway edge lights per AC 150/5340-30.

For straight segments, space taxiway edge lights at 50-foot (15.2 m) longitudinal intervals on straight segments.

Curved taxiway segments require smaller spacing of edge lights. The light spacing is based on the radius of the curve, as described in AC 150/5340-30. Space taxiway edge lights uniformly. On curved edges of more than 30 degrees from point of tangency (PT) of the taxiway section to PT of the intersecting surface, install at least three edge lights. For radii not listed in AC 150/5340-30, determine spacing by linear interpolation.

## 4.13.8 Heliport Identification Beacon.

A heliport identification beacon may be used to provide the pilot with a means of visually locating the heliport. The identification beacon is a flashing white/green/yellow with a rate of 30 to 45 flashes per minute. Install beacons per the guidance below:

Install heliport identification beacons for TRANSPORT heliports.

These beacons are optional for GENERAL AVIATION and HOSPITAL heliports. Beacons at these heliports can be pilot controlled (as an option) such that the beacon is “on” only when needed.

Specify a beacon meeting the guidelines provided by AC 150/5345-12, Specification for Airport and Heliport Beacon.

Locate and install the beacon per AC 150/5340-30.

# Page Intentionally Blank

# CHAPTER 5. Helicopter Facilities on Airports

## 5.1 General.

5.1.1 This chapter addresses design considerations for separate helicopter facilities on airports. Helicopters can operate on airports without interfering with airplane traffic. Operations can occur on existing airport infrastructure (e.g., on airport taxiways) or on dedicated heliport facilities, as shown in Figure 5-1. Separate heliport facilities and approach/departure procedures may be needed when the volume of airplane and/or helicopter traffic affects operations.

5.1.2 At airports with interconnecting passenger traffic between helicopters and airlines, provide gates at the terminal for helicopter boarding. People who use a helicopter to go to an airport generally need convenient access to the airport terminal and the services provided to airplane passengers.

5.1.3 Identify the location of the exclusive-use helicopter facilities, TLOFs, FATOs, safety areas, approach/departure paths, and helicopter taxi routes and taxiways on the ALP. Figure 5-1 shows an example of dedicated heliport facilities located on an airport. Other potential heliport locations are on the roofs of passenger terminals or parking garages serving passenger terminals.

## 5.2 Touchdown and Liftoff Area (TLOF).

Locate the TLOF to provide ready access to the airport terminal or to the helicopter user’s origin or destination. Locate the TLOF away from aircraft movement areas (runways, taxiways, and aircraft parking aprons).

## 5.3 On-Airport Location of Final Approach and Takeoff Area (FATO).

See Table 5-1 for standards of the distance between the centerline of an approach to a runway and the centerline of an approach to a FATO for simultaneous, same direction, VFR operations.

Figure 5-1. Example of Heliport Facilities Located on an Airport  
![0ff39a47afc909a5de6aa531b616153f114d4199891de45622141d0fd6ff4748.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0ff39a47afc909a5de6aa531b616153f114d4199891de45622141d0fd6ff4748.jpg)  
See Table 5-1.

Table 5-1. Recommended Distance between FATO Center to Runway Centerline for VFR Operations
<table><tr><td rowspan=1 colspan=1>Airplane Size</td><td rowspan=1 colspan=1>Small Helicopter7,000 Ibs (3,175 kg)or less</td><td rowspan=1 colspan=1>Medium Helicopter7,001 (3,176 kg) to12,500 Ibs (5,670 kg)</td><td rowspan=1 colspan=1>Large Helicopterover 12,500 Ibs(5,670 kg)</td></tr><tr><td rowspan=1 colspan=1>Small airplane12,500 1bs (5,670 kg)or less</td><td rowspan=1 colspan=1>300 feet(91 m)</td><td rowspan=1 colspan=1>500 feet(152m)</td><td rowspan=1 colspan=1>700 feet(213 m)</td></tr><tr><td rowspan=1 colspan=1>Large airplane12,500 1bs (5,670 kg)to 300,000 1bs(136,079 kg)</td><td rowspan=1 colspan=1>500 feet(152m)</td><td rowspan=1 colspan=1>500feet(152m)</td><td rowspan=1 colspan=1>700 feet(213 m)</td></tr><tr><td rowspan=1 colspan=1>Heavy airplaneOver 300,000 1bs(136,079 kg)</td><td rowspan=1 colspan=1>700 feet(213 m)</td><td rowspan=1 colspan=1>700 feet(213 m)</td><td rowspan=1 colspan=1>700 feet(213 m)</td></tr></table>

## 5.4 Safety Area.

Apply the safety area dimensions and clearances, described in Chapter 2, to heliport facilities being developed on an airport.

## 5.5 VFR Approach/Departure Paths.

To the extent practical, design helicopter approach/departure paths to be independent of approaches to, and departures from, active runways.

## 5.6 Heliport Protection Zone (HPZ).

Establish an HPZ, where practicable, for the airport owner to acquire the land area. Plan the land uses within the HPZ. Where not practicable, the HPZ standards have recommendation status for that portion of the HPZ the airport owner does not control.

## 5.7 Taxiways and Taxi Routes.

When developing exclusive helicopter taxiways or taxi routes at an airport, locate these routes to minimize interaction and/or conflicts with airplane operations. Consider the rotor wash generated by the largest design helicopter anticipated to operate at the facility when determining helicopter taxiway and taxi route distances from airplane operations.

## 5.8 Helicopter Parking.

Locate helicopter parking positions as close to the intended destination or origination of the passengers as conditions and safety permit. See Chapter 3 for guidance on helicopter parking requirements.

## 5.9 Security.

Unless screening was carried out at the helicopter passengers’ departure location, Transportation Security Administration regulations may require that a screening area and/or screening be provided before passengers re-enter the airport’s secured areas. If necessary, establish multiple helicopter parking positions and/or locations in the terminal area to service helicopter passenger screening and/or cargo interconnecting needs. Find information about passenger screening on the Transportation Security Administration website https://www.tsa.gov/public/.

# CHAPTER 6. Instrument Operations

## 6.1 General.

This chapter provides guidance on heliport markings and lighting for GENERAL AVIATION, TRANSPORT, and HOSPITAL heliports. Ensure that at least one of the following visual references is visible or identifiable before the pilot proceeds visually for departure/approach:

FATO lights.

TLOF lights.

Heliport Instrument Lighting System (HILS).

Heliport Approach Lighting System (HALS) or lead-in lights.

Visual Glideslope Indicator (VGSI).

Windsock or windsock light(s). See note below.

Heliport beacon. See note below.

Other facilities or systems approved by the Flight Technologies and Procedures Division (AFS-400).

Locate windsock lights within 500 ft (152 m) of the TLOF.

6.1.1 Instrument flight procedures permit helicopter operations to continue during periods of low cloud ceilings and reduced visibility. Instrument procedures include approach procedures, departure procedures, and missed approach procedures.

6.1.2 The FAA establishes instrument approach procedures under FAA 8260-series Orders overseen by the FAA Flight Procedures and Airspace Group. When a procedure applies to a private (non-public) heliport, is developed for one specific user, or is developed by a non-FAA service provider using unique FAA-approved instrument criteria, the instrument procedure is a “special” instrument procedure. After approval by the FAA, the special instrument procedure is issued to the operator approved to fly the procedure.

6.1.3 See Table 6-1 for instrument approach procedure requirements for precision approaches, non-precision approaches, and approaches to point-in-space.

Table 6-1. Standards for Instrument Approach Procedures
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Precisionapproachto IFRheliport</td><td rowspan=1 colspan=1>Precisionapproachto IFRheliport</td><td rowspan=1 colspan=1>Non-precisionapproach to IFRheliport</td><td rowspan=1 colspan=1>Approach topoint-in-space, proceed|space, proceedvisually</td><td rowspan=1 colspan=1>Approach topoint-in-space, proceed|space, proceedVFR</td></tr><tr><td rowspan=1 colspan=1>Visibilityminimums</td><td rowspan=1 colspan=1>1/4 statuemile(0.4 km)</td><td rowspan=1 colspan=1>1/2 statuemile(0.8 km) 1</td><td rowspan=1 colspan=1>HAL=250-600:1/2statute mile (0.8 km)HAL=601-800: 3/4statute mile (1.2 km)HAL&gt;800: 1 statutemile (1.5 km)</td><td rowspan=1 colspan=1>3/4 statute mile(i(1.2 km) day 6</td><td rowspan=1 colspan=1>3/4 statute mile(1.2 km) day,1 statute mile(1.5 km) night </td></tr><tr><td rowspan=1 colspan=1>Authorizedminima</td><td rowspan=1 colspan=1>≥200 ft(61 m) AGL|i</td><td rowspan=1 colspan=1>≥200(i61 m) AGL</td><td rowspan=1 colspan=1>≥250(76 m) AGL</td><td rowspan=1 colspan=1>≥250(76 m) AGL</td><td rowspan=1 colspan=1>≥250(76 m) AGL</td></tr><tr><td rowspan=1 colspan=1>Heliport type</td><td rowspan=1 colspan=1>IFR</td><td rowspan=1 colspan=1>IFR</td><td rowspan=1 colspan=1>IFR</td><td rowspan=1 colspan=1>VFR</td><td rowspan=1 colspan=1>VFR</td></tr><tr><td rowspan=1 colspan=1>ocs</td><td rowspan=1 colspan=1>34:1 Clear 2i</td><td rowspan=1 colspan=1>34:1 Clear2</td><td rowspan=1 colspan=1>Standard Non-precision ROC</td><td rowspan=1 colspan=1>8:1</td><td rowspan=1 colspan=1>8:1</td></tr><tr><td rowspan=1 colspan=1>Heliport size 5</td><td rowspan=1 colspan=1>Depends ondesignhelicopter</td><td rowspan=1 colspan=1> Depends ondesignhelicopter</td><td rowspan=1 colspan=1>Depends on designhelicopter</td><td rowspan=1 colspan=1>Depends ondesignhelicopter</td><td rowspan=1 colspan=1>Depends ondesignhelicopter</td></tr><tr><td rowspan=1 colspan=1>Heliportmarkings</td><td rowspan=1 colspan=1>SeeChapter 4</td><td rowspan=1 colspan=1>SeeChapter 4</td><td rowspan=1 colspan=1>SeeChapter 4</td><td rowspan=1 colspan=1>SeeChapter 4</td><td rowspan=1 colspan=1>SeeChapter 4</td></tr><tr><td rowspan=1 colspan=1>Heliport lights 3</td><td rowspan=1 colspan=1>Required</td><td rowspan=1 colspan=1>Required</td><td rowspan=1 colspan=1>Required</td><td rowspan=1 colspan=1>Required</td><td rowspan=1 colspan=1>Required</td></tr><tr><td rowspan=1 colspan=1>Survey required</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>No</td></tr><tr><td rowspan=1 colspan=1>Approach lights(HALS)</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td></tr><tr><td rowspan=1 colspan=1>HPZ helicopterprotection</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes</td></tr><tr><td rowspan=1 colspan=1>Final approachreference area</td><td rowspan=1 colspan=1>Yes</td><td rowspan=1 colspan=1>Yes4</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td><td rowspan=1 colspan=1>No</td></tr></table>

1/4 statute mile (0.4 km) reduction authorized with HALS aligned to approach angle and course.  
Minimum glidepath angle of 3 degrees.  
Either TLOF or FATO must be lit at night.  
FARA only required for instrument landing system/localizer-only approaches (ILS/LOC) approaches.  
Minimum heliport size dependent on type of heliport (GENERAL, HOSPITAL, TRANSPORT).  
Proceed visually minimum visibility is 3/4 statute mile (1.2 km) maximum visibility based on distance from missed approach point/descent altitude (MAP/DA) to landing location.  
If HAL greater than 800 ft (244 m) MSL visibility day and night 1 statute mile (1.6 km).

## 6.2 Planning.

This chapter addresses issues that heliport owners consider before requesting the development of instrument approach/departure/missed approach procedures. The standards and recommendations in this AC are not intended to be sufficient to design an instrument procedure. A heliport sponsor should initiate early contact with the appropriate FAA Flight Standards Office to plan for and establish instrument procedures.

## 6.3 Airspace.

Those who design instrument approach/departure/missed approach procedures have some flexibility in the design of such procedures. For this and other reasons, the airspace required to support helicopter instrument approach/departure operations is complex, and it does not lend itself to simple descriptions or the use of figures. Refer to the latest revision of FAA 8260-series Orders for more detailed information on criteria for developing helicopter instrument approach/departure/missed approach procedures.

## 6.4 Final Approach Reference Area (FARA).

For precision instrument procedures only, a certificated helicopter precision approach procedure terminates with the helicopter coming to a hover or touching down within a 150-foot-wide (46 m) by at least 150-foot long (46 m) FARA. The FARA is located at the far end of a 300-foot-wide by 1,225-foot-long (91 m by 373 m) FATO required for a precision instrument procedure. For the purposes of requirements for LBA and lighting, substitute the FARA for the FATO. Figure 6-1 illustrates the FARA/FATO relationship.

Figure 6-1. FARA/FATO Relationship: Precision Instrument Procedure  
![c33cdbde29ef5510df255b645f7d7f1071cad37bc082e913becfa043b01e40d7.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c33cdbde29ef5510df255b645f7d7f1071cad37bc082e913becfa043b01e40d7.jpg)  
The illustrated FARA-FATO relationship is appropriate for a heliport located at an elevation up to 1,000 ft (305 m) above mean sea level.

## 6.5 Improved Instrument Lighting System.

The FAA has not established heliport lighting or helicopter approach lighting standards. Installing lighting systems similar to systems described below may result in lower visibility minimums. Coordinate these systems with Flight Standards and Air Traffic Control (ATC) for all low visibility operations. See Figure 6-2 and Figure 6-3.

## 6.5.1 FATO Perimeter Lighting Enhancement.

Insert an additional elevated green light meeting the standards of Appendix G between each light in the front and rear rows of the elevated perimeter lights to enhance the definition of the FATO.

## 6.5.2 Heliport Instrument Lighting System (HILS).

The HILS consists of 24 unidirectional PAR 56, 200-watt white lights that extend the FATO perimeter lights. The system extends both the right and left edge lights as edge bars and both the front and rear edge lights as wing bars, as shown in Figure 6-2.

## 6.5.2.1 Edge Bars.

Place edge bar lights at 50-foot (15.2 m) intervals, measured from the front and rear row of the FATO perimeter lights.

## 6.5.2.2 Elevated FATO Wing Bars.

Space wing bar lights at 15-foot (4.6 m) intervals, measured from the line of FATO perimeter (side) lights.

## 6.5.2.3 Optional TLOF Lights.

A line of seven white in-pavement lights meeting the standards of Appendix G is optional. Space the lights at 5-foot (1.5 m) intervals in the TLOF pavement. Align the lights on the centerline of the approach course to provide close-in directional guidance and improve TLOF surface definition. These lights are illustrated in Figure 6-2.

## 6.5.3 Heliport Approach Lighting System (HALS).

The HALS depicted in Figure 6-3 is a distinctive approach lighting configuration designed to prevent it from being mistaken for an airport runway approach lighting system.

Figure 6-2. Heliport Instrument Lighting System (HILS): Non-precision  
![6b38ca2f2f253494f1e24089200dab1c32c9fc09dfda515570787d8defe0614c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6b38ca2f2f253494f1e24089200dab1c32c9fc09dfda515570787d8defe0614c.jpg)  
The illustrated HILS installation is appropriate for a minimally sized heliport at an elevation up to 1,000 ft (305 m) above MSL.

Figure 6-3. Heliport Approach Lighting System  
![2dfdc80844c8454bc6d4a6a4cbbfa4fcf0a7bd49aad4df44f12cd7f9620c45f2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2dfdc80844c8454bc6d4a6a4cbbfa4fcf0a7bd49aad4df44f12cd7f9620c45f2.jpg)  
The illustrated heliport approach lighting system (HALS) relationship is appropriate for a heliport located at an elevation up to 1,000 ft (305 m) above mean sea level.  
The illustrated HILS has elevated FATO edge lights. In-pavement FATO edge lights, which are also an option, would be placed just inside the FATO.

## 6.6 Obstacle Evaluation Surfaces.

The instrument procedure developer considers the specific heliport location, its physical characteristics, the terrain, surrounding obstructions, etc., in designing the helicopter instrument approach procedure. Upon development of the instrument procedure, protect the obstacle evaluation surfaces from penetrations. See paragraph 1.1 for additional guidance.

## 6.7 Visual Glideslope Indicators (VGSI).

A VGSI provides pilots with visual vertical course and descent cues. Install the VGSI such that the lowest on-course visual signal provides a minimum of one degree of clearance over any object that lies within ten degrees of the approach course centerline.

## 6.7.1 Siting.

The optimum location of a VGSI is on the extended centerline of the approach path at a distance that brings the helicopter to a hover with the undercarriage between 3 and 8 feet (0.9 to 2.4 m) above the TLOF.

See Figure 6-4 for an illustration of VGSI clearance criteria.

To properly locate the VGSI, estimate the vertical distance from the undercarriage to the pilot’s eye.

## 6.7.2 Control of the VGSI.

Design the VGSI to be pilot controllable such that it is “on” only when needed as an option.

## 6.7.3 VGSI Needed.

A VGSI is an optional feature. However, install a VGSI if one or more of the following conditions exist, especially at night:

Obstacle clearance, noise abatement, or traffic control procedures necessitate a slope to be flown.

The environment of the heliport provides few visual surface cues.

## 6.7.4 Additional Guidance.

Additional guidance is provided in AC 150/5345-52, Generic Visual Glideslope Indicators (GVGI), and AC 150/5345-28, Precision Approach Path Indicator (PAPI) Systems.

Figure 6-4. Visual Glideslope Indicator (VGSI) Siting and Clearance Criteria  
![4bd5b089c0cc9769f5d6b0860f4ae6e79977dae6ed1160c707647576097451bf.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4bd5b089c0cc9769f5d6b0860f4ae6e79977dae6ed1160c707647576097451bf.jpg)

# Page Intentionally Blank

## CHAPTER 7. Heliport Site Safety Elements

## 7.1 General.

This chapter provides guidance on heliport site safety elements which provide enhanced safety for heliport operations.

## 7.2 Marking and Lighting of Difficult-To-See Objects.

Helicopter flight operations require maneuvering near the surface, where nearby obstacles can be a factor whether or not they actually penetrate any approach/departure or transitional surfaces. Objects such as poles, wires, and the high points of buildings are often difficult for a helicopter pilot to identify even in the best daylight conditions, making it difficult to take timely evasive action. Mark and light difficult-to-see objects near any approach/departure surface in accordance with the recommendations provided in AC 70/7460–1, Obstruction Marking and Lighting. Where it is not practical to mark or light an object (such as a tree), consider use of marked and lighted witness poles or low intensity solar obstruction lights.

## 7.2.1 Airspace.

Mark difficult-to-see objects to make them more conspicuous if they penetrate the applicable object identification surfaces, as illustrated in Figure 7-1 and Figure 7-2. Light difficult-to-see objects if a heliport supports operations between dusk and dawn. The object identification surfaces in these two figures are described as follows:

In all directions from the safety area, except under the approach/departure paths, the object identification surface starts at the safety area perimeter and extends out horizontally for 100 feet (30.5 m).

The object identification surface starts from the outside edge of the FATO and extends horizontally out for 800 feet (244 m) along the approach path under the approach/departure surface. The object identification surface extends out for an additional distance of 3,200 feet (975 m) along the approach path while rising on an 8:1 slope (8 units horizontal in 1 unit vertical) from this point. The object identification surface is 100 feet (30.5 m) beneath the approach/departure surface from the point 800 feet (244 m) from the FATO perimeter.

The width of this object identification surface under the approach/departure surface increases as a function of distance from the safety area. The object identification surface extends laterally to a point 100 feet (30.5 m) outside the safety area perimeter from the safety area perimeter. The object identification surface extends laterally 200 feet (61 m) on either side of the approach/departure path at the upper end of the surface.

Figure 7-1. Airspace Where Heliport Marking and Lighting are Recommended: Straight Approach  
![211acfb1c69d189269a03d2f3ab13a7d3f368cee3b233e1bb3da870b5f6fdcf7.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/211acfb1c69d189269a03d2f3ab13a7d3f368cee3b233e1bb3da870b5f6fdcf7.jpg)

Figure 7-2. Airspace Where Heliport Marking and Lighting are Recommended: Curved Approach  
![23dea2f7a3cb68398cb6096c1791bb163fc5a3c7a94a721b4948b64dfe5be193.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/23dea2f7a3cb68398cb6096c1791bb163fc5a3c7a94a721b4948b64dfe5be193.jpg)

## 7.2.2 Shielding of Objects.

Section 77.9, Construction or Alteration Requiring Notice, provides that if there are several objects close together, it may not be necessary to mark all of them if they are shielded. Note that shielding does not apply to objects located on a public-use airport or heliport. Shielding applies only to off-airport objects.

To meet the shielding guidelines, Part 77 requires that an object “be shielded by existing structures of a permanent and substantial nature or by natural terrain or topographic features of equal or greater height and will be located in the congested area of a city, town, or settlement where the shielded structure will not adversely affect safety in air navigation.”

## 7.2.3 Equipment/Object Marking.

Make heliport maintenance and servicing equipment, as well as other objects used in the airside operational areas, conspicuous with paint, reflective paint, reflective tape, or other reflective markings. Reference AC 150/5210-5, Painting, Marking, and Lighting of Vehicles Used on an Airport.

## 7.3 Safety Considerations.

Consider the following safety enhancements in the design of a heliport, as described below. Address other areas, such as the effects of rotor downwash, based on site conditions and the design helicopter.

## 7.3.1 Security.

Provide a heliport with the appropriate means of keeping the operational areas clear of people, animals, and vehicles. Use a method to control access depending upon the helicopter location, type of operation, and types of potential intruders. Follow the guidelines below for use of safety barriers and access control measures:

For ground-level heliports, erect a safety barrier around the helicopter operational areas in the form of a fence or a wall. Other types of safety barriers may be used if they provide adequate positive deterrent to persons inadvertently entering an operational area.

Construct the safety barrier outside of the safety area and below the elevation of the approach/departure and transitional surfaces.

If necessary, near the approach/departure paths, install the barrier well outside the outer perimeter of the safety area.

Ensure any safety barrier is high enough to present a positive deterrent to persons inadvertently entering an operational area but low enough to be non-hazardous to helicopter operations. If the barrier is located under the approach/departure surface, consider lighting the barrier for enhanced visibility for pilots.

For TRANSPORT heliports, control access to airside areas with adequate security measures.

For GENERAL AVIATION and HOSPITAL heliports, control access to airside areas in a manner commensurate with the barrier (for example, build fences with locked gates).

Display a heliport caution sign similar to that shown in Figure 7-3 at all access points.

As an option at HOSPITAL heliports, secure operational areas via the use of security guards and a mixture of fixed and movable barriers.

Figure 7-3. Heliport Caution Sign  
![bb2afe9f2d9ae1d4bf4f3fdad27e33fe8faa560022b4d8e7d1cee932dbfaeafc.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/bb2afe9f2d9ae1d4bf4f3fdad27e33fe8faa560022b4d8e7d1cee932dbfaeafc.jpg)

## 7.3.2 Rescue and Fire Fighting Services.

Heliports are subject to state and local rescue and fire fighting regulations. Provide a fire hose cabinet or extinguisher at each access gate/door and each fueling location. Locate fire hose cabinets, fire extinguishers, and other fire fighting equipment adjacent to, but below the level of, the TLOF (and below the level of the FATO for elevated FATOs at TRANSPORT heliports). See additional guidance in NFPA publications listed in Appendix E.

## 7.3.3 Communications.

Use a Common Traffic Advisory Frequency (CTAF) radio to provide arriving helicopters with heliport and traffic advisory information but do not use this radio to

control air traffic. Contact the Federal Communications Commission (FCC) for information on CTAF licensing.

## 7.3.4 Weather Information.

An automated weather observing system (AWOS) measures and automatically broadcasts current weather conditions at the heliport site. When installing an AWOS, locate it at least 100 feet (30.5 m) and not more than 700 feet (213 m) from the TLOF and such that its instruments will not be affected by rotor wash from helicopter operations. Find guidance on AWOS systems in AC 150/5220-16, Automated Weather Observing Systems (AWOS) for Non-Federal Applications, and FAA Order 6560.20, Siting Criteria for Automated Weather Observing Systems (AWOS). Other weather observing systems will have different siting criteria.

## 7.3.5 Winter Operations.

Swirling snow dispersed by a helicopter’s rotor wash can cause the pilot to lose sight of the intended landing point and/or hide objects that need to be avoided.

Design the heliport to accommodate the methods and equipment to be used for snow removal.

Design the heliport to allow the snow to be removed sufficiently so it will not present an obstruction hazard to the tail rotor, main rotor, or undercarriage.

For heliports subject to winter weather and ice/snow, an optional dark TLOF surface can be used to absorb more heat from the sun and melt residual ice and snow. See paragraph 4.3.4 for guidance on markings for winter operations.

Find guidance on winter operations in AC 150/5200-30, Airport Field Condition Assessments and Winter Operations Safety.

# APPENDIX A. EMERGENCY HELICOPTER LANDING FACILITIES (EHLF)

## A.1 General.

Preplanning emergency landing areas will result in safer and more effective air-support operations. These facilities comprise rooftop emergency facilities and medical emergency sites and are not for routine helicopter operations. Use the following as a guide for developing EHLF facilities.

## A.2 Notification and Coordination.

In addition to any requirements to provide notice under Part 157, advise the local Terminal Approach Radar Control or the local ATC facility manager in writing of the EHLF.

## A.3 Rooftop Emergency Facilities.

Review local building codes to determine if they require structures over a specified height to provide a clear area on the roof capable of accommodating a helicopter to facilitate fire fighting or emergency evacuation operations.

## A.3.1 Building Code Requirements.

State and local building code requirements apply to rooftop facilities. Develop the landing surface to the local fire department requirements based on the size and weight of the helicopter(s) expected to engage in fire or rescue operations (see Figure A-1). Find additional information in various NFPA publications. For additional reference material, see Appendix E.

## A.3.2 TLOF.

Design the TLOF per the following guidelines:

A.3.2.1 Size. Design the TLOF to be square, rectangular, or circular in configuration and centered within the EHLF. Design the length and width or diameter to be at least the controlling dimension D of the largest aircraft expected to use the EHLF.

A.3.2.2 Weight Capacity. Design the TLOF to accommodate the maximum takeoff weight of the design helicopter expected to use the EHLF.

A.3.2.3 Access. Provide two pedestrian access points to the TLOF at least 90 degrees apart with a minimum of 60 feet (18.3 m) TLOF perimeter separation.

## A.3.2.4 Drainage.

Design the surface so drainage flows away from pedestrian access points, with a maximum slope of 1.5 to 2.0 percent.

Figure A-1. Rooftop Emergency Landing Facility  
![a0a3a52e78676d3ebc603597fdbf3b8e8ec6f6127031b6bf0b25c3a689e33a40.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a0a3a52e78676d3ebc603597fdbf3b8e8ec6f6127031b6bf0b25c3a689e33a40.jpg)  
The example shown in the illustration indicates a 9,000 lb (4,082 kg) weight limitation in the center of circle.

## A.3.3 FATO.

Design the FATO to be at the same level as the TLOF.

## A.3.3.1 Size.

Design the FATO to extend a distance of at least 45 feet (13.7 m) in all directions from the center of the EHLF. For safe operation, provide clearance of 0.28 D of the largest helicopter expected but not less than 20 feet (6.1 m) between the helicopter’s main and tail rotor blades and any object that could be struck by these blades.

## A.3.3.2 Obstructions.

As an option, design the FATO to be an imaginary surface outside the TLOF and extending beyond the structure edge. Design the FATO to be unobstructed and without penetration of obstacles such as parapets, window washing equipment, penthouses, handrails, antennas, vents, etc.

## A.3.4 Safety Area.

Provide a clear, unobstructed area, a minimum of 12 feet (3.7 m) wide, on all sides, outside and adjacent to the FATO.

## A.3.5 Safety Net.

If the platform is elevated 4 feet (1.2 m) or more above its surroundings, 29 CFR Section 1910.23, Duty to Have Fall Protection and Falling Object Protection, requires the provision of fall protection. The FAA recommends such protection for all platforms elevated 30 inches (0.8 m) or more. However, do not use permanent railings or fences since they would be safety hazards during helicopter operations. As an option, install a safety net, meeting state and local regulations, but not less than 5 feet (1.5 m) wide. Design the safety net to have a load carrying capability of 25 lbs/sq ft (122 kg/sq m). The net does not project above the level of the TLOF. Fasten both the inside and outside edges of the safety net to a solid structure. Construct nets of materials that are resistant to environmental effects.

## A.3.6 Markings.

## A.3.6.1 TLOF Perimeter.

## A.3.6.2 Touchdown/Positioning Circle (TDPC) Marking.

Center a 12-inch (0.3 m) wide red or orange circular marking, 30 feet (9.1 m) in diameter, within the TLOF. Use a contrasting color for the background within the circle.

## A.3.6.3 Weight Capacity.

Mark the TLOF with the maximum takeoff weight of the design helicopter, in units of thousands of pounds (for example, a number “9”

indicating 9,000 lbs (4,082 kg) GW), with each numeral ten feet (3 m) in height, centered within the TLOF.

## A.3.6.4 Markings for Pedestrians.

Clearly mark rooftop access paths, EHLF access paths, and assembly zone(s) with surface paint and instructional signage.

## A.3.7 Access.

## A.3.7.1 Stairs.

Provide a minimum of two rooftop access stairs, with no less than 150 degrees separation, connecting to the top floor of the structure, with at least one providing access to the structure’s emergency staircase.

## A.3.7.2 Doors.

Always keep the penthouse and stairwell rooftop access doors unlocked to provide access to the EHLF. As an option, equip doors with “panic bar” hardware and/or alarm them.

## A.3.8 Wind Cone.

Install a wind cone assembly conforming to AC 150/5345-27 to show the direction and magnitude of the wind. Ensure it is an orange wind cone within the line-of-sight from the EHLF and outside the approach/departure path(s).

## A.3.9 Lighting.

Shield ambient rooftop lighting to avoid affecting the pilot’s vision.

## APPENDIX B. PRE-DESIGNATED EMERGENCY LANDING AREAS (PELAS)

Pre-designated emergency landing areas (PELAs) are clear and level areas near the scene of an accident or incident that the local emergency response team designates as the place where the helicopter air ambulance is directed to land to transport an injured person to a hospital. Provide such sites in various locations within a jurisdiction to support fast response to medical emergencies and accidents. Pre-designating these areas provides the opportunity to inspect potential sites in advance and to select sites that have adequate clear approach/departure airspace and adequate clear ground space. See the Aeronautical Information Manual (AIM), Chapter 10, for guidance on setting up offsite scene or PELA landing sites.

## Page Intentionally Blank

## APPENDIX C. HELICOPTER DATA

This appendix contains selected helicopter data needed by a heliport designer. These data represent the most critical weight, dimensional, or other data entry for that helicopter model, recognizing that specific versions of the model may weigh less, be smaller in some features, carry fewer passengers, etc.

Various helicopter manufacturers have provided this information. Confirm data by contacting the manufacturer(s) of the specific helicopter(s) of interest.

Legend for Figure C-1 and Table C-1: Helicopter Dimensions and Data
<table><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>Manufacturer name and helicopter model</td></tr><tr><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>Maximum takeoff weight in pounds</td></tr><tr><td rowspan=1 colspan=1>D</td><td rowspan=1 colspan=1>Controlling dimension</td></tr><tr><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>Number of blades</td></tr><tr><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>Rotor plane clearance in feet</td></tr><tr><td rowspan=1 colspan=1>H</td><td rowspan=1 colspan=1>Overall height in feet (usually at tail rotor)</td></tr><tr><td rowspan=1 colspan=1>I</td><td rowspan=1 colspan=1>Tail rotor diameter (in feet)</td></tr><tr><td rowspan=1 colspan=1>J</td><td rowspan=1 colspan=1>Number of tail rotor blades</td></tr><tr><td rowspan=1 colspan=1>K</td><td rowspan=1 colspan=1>Tail rotor ground clearance in feet</td></tr><tr><td rowspan=1 colspan=1>L</td><td rowspan=1 colspan=1>Type of undercarriage</td></tr><tr><td rowspan=1 colspan=1>M</td><td rowspan=1 colspan=1>Number and type of engines</td></tr><tr><td rowspan=1 colspan=1>N</td><td rowspan=1 colspan=1>Number of crew and passengers</td></tr><tr><td rowspan=1 colspan=1>OL</td><td rowspan=1 colspan=1>Overall helicopter length in feet (rotors at their maximum extension)</td></tr><tr><td rowspan=1 colspan=1>oW</td><td rowspan=1 colspan=1>Overall aircraft width in feet</td></tr><tr><td rowspan=1 colspan=1>RD</td><td rowspan=1 colspan=1>Rotor diameter in feet</td></tr><tr><td rowspan=1 colspan=1>TR</td><td rowspan=1 colspan=1>Distance from rotor hub to tip of tail rotor in feet</td></tr><tr><td rowspan=1 colspan=1>UCL</td><td rowspan=1 colspan=1>Undercarriage length in feet</td></tr><tr><td rowspan=1 colspan=1>UCW</td><td rowspan=1 colspan=1> Undercarriage width in feet (the distance between the outside edges ofthe tires or the skids)</td></tr></table>

Figure C-1. Helicopter Dimensions  
![7e264aaf427a4529437625a046975534bbb4e676378e89e7685f4844a88a0752.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7e264aaf427a4529437625a046975534bbb4e676378e89e7685f4844a88a0752.jpg)

Table C-1. Helicopter Data
<table><tr><td rowspan=2 colspan=1>Manufacturer/Model</td><td rowspan=2 colspan=1>M HoayeL unuxeN</td><td rowspan=2 colspan=1>(4}) uojsuug uo.uo</td><td rowspan=2 colspan=1>(H) uuT Ie.AO</td><td rowspan=2 colspan=1>() u!H IR.AO</td><td rowspan=1 colspan=4>Main Rotor</td><td rowspan=1 colspan=3>Tail Rotor</td><td rowspan=1 colspan=3>Undercarriage</td><td rowspan=2 colspan=1>/su3ug Jo JaqunNadL</td><td rowspan=2 colspan=1>/.0qunN Ma.DJaqunN xed</td></tr><tr><td rowspan=1 colspan=1>(H) Jauna</td><td rowspan=1 colspan=1>sopeia Jo aqunN</td><td rowspan=1 colspan=1>E pun0.15</td><td rowspan=1 colspan=1>(H) sn!pey</td><td rowspan=1 colspan=1>(H) .uRa</td><td rowspan=1 colspan=1>sapeia Jo aqunN</td><td rowspan=1 colspan=1>田puno.</td><td rowspan=1 colspan=1>adKI</td><td rowspan=1 colspan=1>() q8uT</td><td rowspan=1 colspan=1>() up!M</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>D</td><td rowspan=1 colspan=1>OL</td><td rowspan=1 colspan=1>H</td><td rowspan=1 colspan=1>RD</td><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>TR</td><td rowspan=1 colspan=1>I</td><td rowspan=1 colspan=1>J</td><td rowspan=1 colspan=1>K</td><td rowspan=1 colspan=1>L</td><td rowspan=1 colspan=1>UCL</td><td rowspan=1 colspan=1>UCW</td><td rowspan=1 colspan=1>M</td><td rowspan=1 colspan=1>N</td></tr><tr><td rowspan=1 colspan=1>AgustaWestland</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>A-109A</td><td rowspan=1 colspan=1>5,732</td><td rowspan=1 colspan=1>42.8</td><td rowspan=1 colspan=1>42.8</td><td rowspan=1 colspan=1>11.2</td><td rowspan=1 colspan=1>36.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>6.7</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.3</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>11.6</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1-2&amp;6-7</td></tr><tr><td rowspan=1 colspan=1>A-119 Koala</td><td rowspan=1 colspan=1>5,997</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>12.4</td><td rowspan=1 colspan=1>36.6</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>25.5</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>4.2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>13.4</td><td rowspan=1 colspan=1>5.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;6-7</td></tr><tr><td rowspan=1 colspan=1>AW-109E Power</td><td rowspan=1 colspan=1>6,283</td><td rowspan=1 colspan=1>42.8</td><td rowspan=1 colspan=1>42.8</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>36.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>7.1</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>187</td></tr><tr><td rowspan=1 colspan=1>AW-109S Grand</td><td rowspan=1 colspan=1>7,000</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>11.2</td><td rowspan=1 colspan=1>35.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.3</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>12.3</td><td rowspan=1 colspan=1>7.1</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1-2&amp;6-7</td></tr><tr><td rowspan=1 colspan=1>AW-119 Ke</td><td rowspan=1 colspan=1>6,283</td><td rowspan=1 colspan=1>42.4</td><td rowspan=1 colspan=1>42.4</td><td rowspan=1 colspan=1>11.8</td><td rowspan=1 colspan=1>35.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.3</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.8</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>11.1</td><td rowspan=1 colspan=1>7</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>186-7</td></tr><tr><td rowspan=1 colspan=1>AW-139</td><td rowspan=1 colspan=1>14,991</td><td rowspan=1 colspan=1>54.7</td><td rowspan=1 colspan=1>54.7</td><td rowspan=1 colspan=1>16.4</td><td rowspan=1 colspan=1>42.6</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>12.9</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>8.9</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>14.2</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1-28&amp;15</td></tr><tr><td rowspan=1 colspan=1>AW-101</td><td rowspan=1 colspan=1>34,392</td><td rowspan=1 colspan=1>74.8</td><td rowspan=1 colspan=1>74.8</td><td rowspan=1 colspan=1>21.7</td><td rowspan=1 colspan=1>61</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>15.4</td><td rowspan=1 colspan=1>45</td><td rowspan=1 colspan=1>13.1</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>8.4</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>14.8</td><td rowspan=1 colspan=1>3-T</td><td rowspan=1 colspan=1>3&amp;30</td></tr><tr><td rowspan=1 colspan=1>Westland WG30</td><td rowspan=1 colspan=1>12,800</td><td rowspan=1 colspan=1>52.2</td><td rowspan=1 colspan=1>52.2</td><td rowspan=1 colspan=1>15.5</td><td rowspan=1 colspan=1>43.7</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>12.5</td><td rowspan=1 colspan=1>31</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>17.9</td><td rowspan=1 colspan=1>10.1</td><td rowspan=1 colspan=1>2+T</td><td rowspan=1 colspan=1>2&amp;19</td></tr><tr><td rowspan=1 colspan=1>Bell Helicopter</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>47G</td><td rowspan=1 colspan=1>2,950</td><td rowspan=1 colspan=1>43.6</td><td rowspan=1 colspan=1>43.6</td><td rowspan=1 colspan=1>9.3</td><td rowspan=1 colspan=1>37.1</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>6.1</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.9</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>182-3</td></tr><tr><td rowspan=1 colspan=1>205B, UH-1H,Huey I, 210</td><td rowspan=1 colspan=1>10,500</td><td rowspan=1 colspan=1>57.8</td><td rowspan=1 colspan=1>57.8</td><td rowspan=1 colspan=1>14.5</td><td rowspan=1 colspan=1>48</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>7.3</td><td rowspan=1 colspan=1>33.1</td><td rowspan=1 colspan=1>8.5</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>5.9</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>12.1</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;14</td></tr><tr><td rowspan=1 colspan=1>206B-1,2,3</td><td rowspan=1 colspan=1>3,350</td><td rowspan=1 colspan=1>39.2</td><td rowspan=1 colspan=1>39.2</td><td rowspan=1 colspan=1>10.8</td><td rowspan=1 colspan=1>33.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>22.5</td><td rowspan=1 colspan=1>5.2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>6.7</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>206L-1,3,4</td><td rowspan=1 colspan=1>4,450</td><td rowspan=1 colspan=1>42.4</td><td rowspan=1 colspan=1>42.4</td><td rowspan=1 colspan=1>10.9</td><td rowspan=1 colspan=1>37</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>24</td><td rowspan=1 colspan=1>5.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.9</td><td rowspan=1 colspan=1>7.7</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>186</td></tr><tr><td rowspan=1 colspan=1>212</td><td rowspan=1 colspan=1>11,200</td><td rowspan=1 colspan=1>57.3</td><td rowspan=1 colspan=1>57.3</td><td rowspan=1 colspan=1>14.9</td><td rowspan=1 colspan=1>48.2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>22.2</td><td rowspan=1 colspan=1>8.5</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>12.1</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1814</td></tr><tr><td rowspan=1 colspan=1>214ST</td><td rowspan=1 colspan=1>17,500</td><td rowspan=1 colspan=1>62.2</td><td rowspan=1 colspan=1>62.2</td><td rowspan=1 colspan=1>15.9</td><td rowspan=1 colspan=1>52</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>37</td><td rowspan=1 colspan=1>9.7</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>wheel/skid</td><td rowspan=1 colspan=1>12.1</td><td rowspan=1 colspan=1>8.6</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;16-17</td></tr><tr><td rowspan=1 colspan=1>222B,UT</td><td rowspan=1 colspan=1>8,250</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>12.2</td><td rowspan=1 colspan=1>42</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>29.2</td><td rowspan=1 colspan=1>6.9</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.7</td><td rowspan=1 colspan=1>wheel/skid</td><td rowspan=1 colspan=1>12.2</td><td rowspan=1 colspan=1>7.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;9</td></tr><tr><td rowspan=1 colspan=1>230</td><td rowspan=1 colspan=1>8,400</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>11.7</td><td rowspan=1 colspan=1>42</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>29.2</td><td rowspan=1 colspan=1>6.9</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.7</td><td rowspan=1 colspan=1>whee/skid</td><td rowspan=1 colspan=1>12.2</td><td rowspan=1 colspan=1>7.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;9</td></tr><tr><td rowspan=1 colspan=1>407</td><td rowspan=1 colspan=1>5,250</td><td rowspan=1 colspan=1>41.4</td><td rowspan=1 colspan=1>41.4</td><td rowspan=1 colspan=1>10.2</td><td rowspan=1 colspan=1>35</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>7.8</td><td rowspan=1 colspan=1>24.3</td><td rowspan=1 colspan=1>5.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.9</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;6</td></tr><tr><td rowspan=1 colspan=1>412EP, SP, HP</td><td rowspan=1 colspan=1>11,900</td><td rowspan=1 colspan=1>56.2</td><td rowspan=1 colspan=1>56.2</td><td rowspan=1 colspan=1>14.9</td><td rowspan=1 colspan=1>46</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>34</td><td rowspan=1 colspan=1>8.6</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>4.8</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>12.1</td><td rowspan=1 colspan=1>9.5</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;14</td></tr><tr><td rowspan=1 colspan=1>427VFR</td><td rowspan=1 colspan=1>6.,550</td><td rowspan=1 colspan=1>42.6</td><td rowspan=1 colspan=1>42.6</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1>37</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>24.1</td><td rowspan=1 colspan=1>5.7</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;7</td></tr><tr><td rowspan=1 colspan=1>429</td><td rowspan=1 colspan=1>7,000</td><td rowspan=1 colspan=1>43</td><td rowspan=1 colspan=1>43</td><td rowspan=1 colspan=1>13.3</td><td rowspan=1 colspan=1>36</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8.5</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>5.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.9</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>187</td></tr><tr><td rowspan=1 colspan=1>430</td><td rowspan=1 colspan=1>9,300</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>50.3</td><td rowspan=1 colspan=1>13.3</td><td rowspan=1 colspan=1>42</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1>29.2</td><td rowspan=1 colspan=1>6.9</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.7</td><td rowspan=1 colspan=1>wheel/skid</td><td rowspan=1 colspan=1>12.4</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;9</td></tr></table>

Appendix C

<table><tr><td rowspan=2 colspan=1>Manufacturer/Model</td><td rowspan=2 colspan=1>uM HoayeL unxe</td><td rowspan=2 colspan=1>(4) uoisuna Suo.u</td><td rowspan=2 colspan=1>(4) y8uT I.1AO</td><td rowspan=2 colspan=1>(H) u8!H IE.1AO</td><td rowspan=1 colspan=4>Main Rotor</td><td rowspan=1 colspan=3>Tail Rotor</td><td rowspan=1 colspan=3>Undercarriage</td><td rowspan=2 colspan=1>/sau8ug Jo .IqunNadkL</td><td rowspan=2 colspan=1>/aqunN MaD.aqunN xed</td></tr><tr><td rowspan=1 colspan=1>(H) na</td><td rowspan=1 colspan=1>sopeia Jo JaqunN</td><td rowspan=1 colspan=1>ea puno.5()</td><td rowspan=1 colspan=1>() snipey</td><td rowspan=1 colspan=1>(H) 1guer!a</td><td rowspan=1 colspan=1>sop ia Jo .aqunN</td><td rowspan=1 colspan=1>ue.ean puno.5四</td><td rowspan=1 colspan=1>adKL</td><td rowspan=1 colspan=1>(4) u8uaT</td><td rowspan=1 colspan=1>() up!M</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>D</td><td rowspan=1 colspan=1>OL</td><td rowspan=1 colspan=1>H</td><td rowspan=1 colspan=1>RD</td><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>TR</td><td rowspan=1 colspan=1>I</td><td rowspan=1 colspan=1>J</td><td rowspan=1 colspan=1>K</td><td rowspan=1 colspan=1>L</td><td rowspan=1 colspan=1>UCL</td><td rowspan=1 colspan=1>UCW</td><td rowspan=1 colspan=1>M</td><td rowspan=1 colspan=1>N</td></tr><tr><td rowspan=1 colspan=1>Boeing</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>107/CH-46E</td><td rowspan=1 colspan=1>24,300</td><td rowspan=1 colspan=1>84.3</td><td rowspan=1 colspan=1>84.3</td><td rowspan=1 colspan=1>16.7</td><td rowspan=1 colspan=1>51</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>15</td><td rowspan=1 colspan=1>59</td><td rowspan=1 colspan=1>51</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>17</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>24.9</td><td rowspan=1 colspan=1>14.5</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>3&amp;25</td></tr><tr><td rowspan=1 colspan=1>234/CH-47F/G</td><td rowspan=1 colspan=1>54,000</td><td rowspan=1 colspan=1>99</td><td rowspan=1 colspan=1>99</td><td rowspan=1 colspan=1>19</td><td rowspan=1 colspan=1>60</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>69</td><td rowspan=1 colspan=1>60</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>19</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>22.5</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>3&amp;44</td></tr><tr><td rowspan=1 colspan=1>Brantly/Hynes</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>B-2B</td><td rowspan=1 colspan=1>1,670</td><td rowspan=1 colspan=1>28.1</td><td rowspan=1 colspan=1>28.1</td><td rowspan=1 colspan=1>6.9</td><td rowspan=1 colspan=1>23.8</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>4.8</td><td rowspan=1 colspan=1>16</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>6.8</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;1</td></tr><tr><td rowspan=1 colspan=1>305</td><td rowspan=1 colspan=1>2,900</td><td rowspan=1 colspan=1>32.9</td><td rowspan=1 colspan=1>32.9</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>28.7</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>19</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>wheel/skid</td><td rowspan=1 colspan=1>6.2</td><td rowspan=1 colspan=1>6.8</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>Enstrom</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>F-28F/280FX</td><td rowspan=1 colspan=1>2,600</td><td rowspan=1 colspan=1>29.3</td><td rowspan=1 colspan=1>29.3</td><td rowspan=1 colspan=1>9</td><td rowspan=1 colspan=1>32</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>20.6</td><td rowspan=1 colspan=1>4.7</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>7.3</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;2</td></tr><tr><td rowspan=1 colspan=1>480B/TH-28</td><td rowspan=1 colspan=1>3,000</td><td rowspan=1 colspan=1>30.1</td><td rowspan=1 colspan=1>30.1</td><td rowspan=1 colspan=1>9.7</td><td rowspan=1 colspan=1>32</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>21.2</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.6</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>Erickson</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>S-64E/F AirCrane</td><td rowspan=1 colspan=1>42,000-4700</td><td rowspan=1 colspan=1>88.5</td><td rowspan=1 colspan=1>88.5</td><td rowspan=1 colspan=1>25.4</td><td rowspan=1 colspan=1>72</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>15.7</td><td rowspan=1 colspan=1>53</td><td rowspan=1 colspan=1>16</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.4</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>24.4</td><td rowspan=1 colspan=1>19.9</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>3&amp;0</td></tr><tr><td rowspan=1 colspan=1>Eurocopter</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>SA-315 Lama</td><td rowspan=1 colspan=1>5,070</td><td rowspan=1 colspan=1>42.3</td><td rowspan=1 colspan=1>42.3</td><td rowspan=1 colspan=1>10.2</td><td rowspan=1 colspan=1>36.2</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>10.1</td><td rowspan=1 colspan=1>20</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>3.2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>10.8</td><td rowspan=1 colspan=1>7.8</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>184</td></tr><tr><td rowspan=1 colspan=1>SA-316/319Alouette</td><td rowspan=1 colspan=1>4,850</td><td rowspan=1 colspan=1>33.4</td><td rowspan=1 colspan=1>33.4</td><td rowspan=1 colspan=1>9.7</td><td rowspan=1 colspan=1>36.1</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>27.7</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>2.8</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>8.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>SA-330 Puma</td><td rowspan=1 colspan=1>16,315</td><td rowspan=1 colspan=1>59.6</td><td rowspan=1 colspan=1>59.6</td><td rowspan=1 colspan=1>16.9</td><td rowspan=1 colspan=1>49.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>14.4</td><td rowspan=1 colspan=1>35</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>13.3</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;20</td></tr><tr><td rowspan=1 colspan=1>SA/AS-332, SuperPuma</td><td rowspan=1 colspan=1>20,172</td><td rowspan=1 colspan=1>61.3</td><td rowspan=1 colspan=1>61.3</td><td rowspan=1 colspan=1>16.3</td><td rowspan=1 colspan=1>53.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>14.6</td><td rowspan=1 colspan=1>36</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>7.1</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>17.3</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;24</td></tr><tr><td rowspan=1 colspan=1>SA-341/342Gazelle</td><td rowspan=1 colspan=1>4,100</td><td rowspan=1 colspan=1>39.3</td><td rowspan=1 colspan=1>39.3</td><td rowspan=1 colspan=1>10.2</td><td rowspan=1 colspan=1>34.5</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>8.9</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>2.4</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>6.6</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>AS-350 A Star</td><td rowspan=1 colspan=1>4,960</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>35.1</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>10.6</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>6.1</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>4.7</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;6</td></tr><tr><td rowspan=1 colspan=1>AS-355 Twin Star</td><td rowspan=1 colspan=1>5,732</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>42.5</td><td rowspan=1 colspan=1>9.9</td><td rowspan=1 colspan=1>35.9</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>10.3</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>6.1</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.6</td><td rowspan=1 colspan=1>7.1</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;6</td></tr><tr><td rowspan=1 colspan=1>AS-360 Dauphin</td><td rowspan=1 colspan=1>6,600</td><td rowspan=1 colspan=1>43.3</td><td rowspan=1 colspan=1>43.3</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>37.7</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>10.7</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>2.6</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>23.7</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;13</td></tr><tr><td rowspan=1 colspan=1>AS-365Dauphin/H-65Dolphin</td><td rowspan=1 colspan=1>9,480</td><td rowspan=1 colspan=1>45.1</td><td rowspan=1 colspan=1>45.1</td><td rowspan=1 colspan=1>13.3</td><td rowspan=1 colspan=1>39.2</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11.4</td><td rowspan=1 colspan=1>24</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>2.6</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>11.9</td><td rowspan=1 colspan=1>6.2</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;11</td></tr><tr><td rowspan=1 colspan=1>BO-105</td><td rowspan=1 colspan=1>5,732</td><td rowspan=1 colspan=1>38.9</td><td rowspan=1 colspan=1>38.9</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>32.3</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>6.2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;5</td></tr><tr><td rowspan=1 colspan=1>BK-117</td><td rowspan=1 colspan=1>7,385</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>12.6</td><td rowspan=1 colspan=1>36.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>25</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>11.6</td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;10</td></tr><tr><td rowspan=1 colspan=1>EC-120</td><td rowspan=1 colspan=1>3,780</td><td rowspan=1 colspan=1>37.8</td><td rowspan=1 colspan=1>37.8</td><td rowspan=1 colspan=1>11.2</td><td rowspan=1 colspan=1>32.8</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>10.1</td><td rowspan=1 colspan=1>24.6</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>2.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.4</td><td rowspan=1 colspan=1>6.8</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>EC-130</td><td rowspan=1 colspan=1>5,291</td><td rowspan=1 colspan=1>41.5</td><td rowspan=1 colspan=1>41.5</td><td rowspan=1 colspan=1>11.8</td><td rowspan=1 colspan=1>35.1</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>23.7</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>5.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1>7.9</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;7</td></tr></table>

Appendix C

<table><tr><td rowspan=2 colspan=1>Manufacturer/Model</td><td rowspan=2 colspan=1>M HoL un</td><td rowspan=2 colspan=1>(4) uoisuna Suo.u</td><td rowspan=2 colspan=1>(4) q8uT I.1AO</td><td rowspan=2 colspan=1>(H) u !H IE.IAO</td><td rowspan=1 colspan=4>Main Rotor</td><td rowspan=1 colspan=3>Tail Rotor</td><td rowspan=1 colspan=3>Undercarriage</td><td rowspan=2 colspan=1>/sou3ug Jo qunNadkL</td><td rowspan=2 colspan=1>/aqunN MaDJaqunN xed</td></tr><tr><td rowspan=1 colspan=1>(H) Jea</td><td rowspan=1 colspan=1>sapeia jo .squnN</td><td rowspan=1 colspan=1>uean pno.15(4)</td><td rowspan=1 colspan=1>() snpe</td><td rowspan=1 colspan=1>(H) spuer</td><td rowspan=1 colspan=1>sapea o aqunn</td><td rowspan=1 colspan=1>e puonm</td><td rowspan=1 colspan=1>adsI</td><td rowspan=1 colspan=1>(4}) qöuaT</td><td rowspan=1 colspan=1>() up!M</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>D</td><td rowspan=1 colspan=1>OL</td><td rowspan=1 colspan=1>H</td><td rowspan=1 colspan=1>RD</td><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>TR</td><td rowspan=1 colspan=1>I</td><td rowspan=1 colspan=1>J</td><td rowspan=1 colspan=1>K</td><td rowspan=1 colspan=1>L</td><td rowspan=1 colspan=1>UCL</td><td rowspan=1 colspan=1>UCW</td><td rowspan=1 colspan=1>M</td><td rowspan=1 colspan=1>N</td></tr><tr><td rowspan=1 colspan=1>EC-135</td><td rowspan=1 colspan=1>6,250</td><td rowspan=1 colspan=1>40</td><td rowspan=1 colspan=1>40</td><td rowspan=1 colspan=1>11.5</td><td rowspan=1 colspan=1>33.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>22.8</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>5.6</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1>6.6</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;6</td></tr><tr><td rowspan=1 colspan=1>EC-145/UH-72A</td><td rowspan=1 colspan=1>7,904</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>42.7</td><td rowspan=1 colspan=1>13</td><td rowspan=1 colspan=1>36.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11.3</td><td rowspan=1 colspan=1>28</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>10.7</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>9.5</td><td rowspan=1 colspan=1>7.9</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1&amp;8</td></tr><tr><td rowspan=1 colspan=1>EC-155</td><td rowspan=1 colspan=1>10,692</td><td rowspan=1 colspan=1>46.9</td><td rowspan=1 colspan=1>46.9</td><td rowspan=1 colspan=1>14.27</td><td rowspan=1 colspan=1>41.3</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>12</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>Fenestron</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>3.1</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>12.8</td><td rowspan=1 colspan=1>6.2</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2812</td></tr><tr><td rowspan=1 colspan=1>EC-225</td><td rowspan=1 colspan=1>24,332</td><td rowspan=1 colspan=1>64</td><td rowspan=1 colspan=1>64</td><td rowspan=1 colspan=1>16.3</td><td rowspan=1 colspan=1>53.1</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>15.1</td><td rowspan=1 colspan=1>38</td><td rowspan=1 colspan=1>10.3</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>17.2</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2824</td></tr><tr><td rowspan=1 colspan=1>Kaman</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>K-Max/K1200</td><td rowspan=1 colspan=1>7,000</td><td rowspan=1 colspan=1>52</td><td rowspan=1 colspan=1>52</td><td rowspan=1 colspan=1>21</td><td rowspan=1 colspan=1>48.2</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>10.7</td><td rowspan=1 colspan=1>28</td><td rowspan=1 colspan=1>n</td><td rowspan=1 colspan=1>a</td><td rowspan=1 colspan=1>n/a</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>15.3</td><td rowspan=1 colspan=1>11.3</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;0</td></tr><tr><td rowspan=1 colspan=1>SH-2G Seasprite</td><td rowspan=1 colspan=1>14,200d</td><td rowspan=1 colspan=1>52.5</td><td rowspan=1 colspan=1>52.5</td><td rowspan=1 colspan=1>15.1</td><td rowspan=1 colspan=1>44</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>388</td></tr><tr><td rowspan=1 colspan=1>MD Helicopters</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>500E</td><td rowspan=1 colspan=1>3,000</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>8.4</td><td rowspan=1 colspan=1>26.4</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>4.6</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>184</td></tr><tr><td rowspan=1 colspan=1>530F</td><td rowspan=1 colspan=1>3,100</td><td rowspan=1 colspan=1>32.1</td><td rowspan=1 colspan=1>32.1</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>27.4</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>19</td><td rowspan=1 colspan=1>4.8</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>1.3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>520N</td><td rowspan=1 colspan=1>3,350</td><td rowspan=1 colspan=1>32.1</td><td rowspan=1 colspan=1>32.1</td><td rowspan=1 colspan=1>9.7</td><td rowspan=1 colspan=1>27.4</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>17</td><td rowspan=1 colspan=1>NOTAR</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>n/a</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.1</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>600N</td><td rowspan=1 colspan=1>4,100</td><td rowspan=1 colspan=1>36.9</td><td rowspan=1 colspan=1>36.9</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>27.5</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>NOTAR</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>n/a</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>10.1</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;7</td></tr><tr><td rowspan=1 colspan=1>Explorer/ 902</td><td rowspan=1 colspan=1>6,500</td><td rowspan=1 colspan=1>38.8</td><td rowspan=1 colspan=1>38.8</td><td rowspan=1 colspan=1>12</td><td rowspan=1 colspan=1>33.8</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>12</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>NOTAR</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>n/a</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>7.3</td><td rowspan=1 colspan=1>7.3</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>1-2&amp;6-7</td></tr><tr><td rowspan=1 colspan=1>Robinson</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>R-22 Beta</td><td rowspan=1 colspan=1>1,370</td><td rowspan=1 colspan=1>28.8</td><td rowspan=1 colspan=1>28.8</td><td rowspan=1 colspan=1>8.9</td><td rowspan=1 colspan=1>25.2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>16</td><td rowspan=1 colspan=1>3.5</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>4.1</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>4.2</td><td rowspan=1 colspan=1>6.3</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>181</td></tr><tr><td rowspan=1 colspan=1>R-44 Raven</td><td rowspan=1 colspan=1>2,500</td><td rowspan=1 colspan=1>38.3</td><td rowspan=1 colspan=1>38.3</td><td rowspan=1 colspan=1>10.8</td><td rowspan=1 colspan=1>33</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1>22</td><td rowspan=1 colspan=1>4.8</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.8</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>4.2</td><td rowspan=1 colspan=1>7.2</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;3</td></tr><tr><td rowspan=1 colspan=1>R-66 Turbine</td><td rowspan=1 colspan=1>2,700</td><td rowspan=1 colspan=1>38.3</td><td rowspan=1 colspan=1>38.3</td><td rowspan=1 colspan=1>11.4</td><td rowspan=1 colspan=1>33</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>10.5</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.6</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>4.2</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>Fairchild-Hiller/Rogerson-Hiller</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>360/UH-12/OH-23</td><td rowspan=1 colspan=1>3,100</td><td rowspan=1 colspan=1>40.8</td><td rowspan=1 colspan=1>40.8</td><td rowspan=1 colspan=1>10.2</td><td rowspan=1 colspan=1>35.4</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>10.1</td><td rowspan=1 colspan=1>23</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>7.5</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;3</td></tr><tr><td rowspan=1 colspan=1>FH/RH-1100</td><td rowspan=1 colspan=1>3,500</td><td rowspan=1 colspan=1>41.3</td><td rowspan=1 colspan=1>41.3</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>35.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>9.5</td><td rowspan=1 colspan=1>24</td><td rowspan=1 colspan=1>6</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>7.9</td><td rowspan=1 colspan=1>7.2</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>1&amp;4</td></tr><tr><td rowspan=1 colspan=1>Sikorsky/Schweizer</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>HU-269A/A-1/B,TH55A</td><td rowspan=1 colspan=1>1,850</td><td rowspan=1 colspan=1>29</td><td rowspan=1 colspan=1>29</td><td rowspan=1 colspan=1>9</td><td rowspan=1 colspan=1>26</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>8.8</td><td rowspan=1 colspan=1>15</td><td rowspan=1 colspan=1>3.8</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.5</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;1</td></tr><tr><td rowspan=1 colspan=1>300C</td><td rowspan=1 colspan=1>2,050</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>8.7</td><td rowspan=1 colspan=1>26.8</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>8.7</td><td rowspan=1 colspan=1>15.3</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.8</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;2</td></tr><tr><td rowspan=1 colspan=1>300CB/CBi</td><td rowspan=1 colspan=1>1,750</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>30.8</td><td rowspan=1 colspan=1>8.7</td><td rowspan=1 colspan=1>26.8</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>8.7</td><td rowspan=1 colspan=1>15.3</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>2.8</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>1-P</td><td rowspan=1 colspan=1>1&amp;1</td></tr><tr><td rowspan=1 colspan=1>330/330SP/333</td><td rowspan=1 colspan=1>2,550</td><td rowspan=1 colspan=1>31.2</td><td rowspan=1 colspan=1>31.2</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>27.5</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>15.3</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>182-3</td></tr><tr><td rowspan=1 colspan=1>S-434</td><td rowspan=1 colspan=1>2,900</td><td rowspan=1 colspan=1>31.2</td><td rowspan=1 colspan=1>31.2</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>27.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.2</td><td rowspan=1 colspan=1>15.3</td><td rowspan=1 colspan=1>4.3</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>3.2</td><td rowspan=1 colspan=1>skid</td><td rowspan=1 colspan=1>8.3</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>182-3</td></tr></table>

Appendix C

<table><tr><td rowspan=2 colspan=1>Manufacturer/Model</td><td rowspan=2 colspan=1>a HoayeL unuxen</td><td rowspan=2 colspan=1>(4) uoisua uou</td><td rowspan=2 colspan=1>() uuT IAO</td><td rowspan=2 colspan=1>(H)  I.AO</td><td rowspan=1 colspan=4>Main Rotor</td><td rowspan=1 colspan=3>Tail Rotor</td><td rowspan=1 colspan=3>Undercarriage</td><td rowspan=2 colspan=1>/sou3ua J0 NqunNadkL</td><td rowspan=2 colspan=1>/.3qunN ma.DJaqunN xed</td></tr><tr><td rowspan=1 colspan=1>(H) Jwna</td><td rowspan=1 colspan=1>sapeia o aqunN</td><td rowspan=1 colspan=1>aee puno国</td><td rowspan=1 colspan=1>() snipey</td><td rowspan=1 colspan=1>() .Iuea</td><td rowspan=1 colspan=1>sapeia o aqunn</td><td rowspan=1 colspan=1>ueeaiS puno.s国</td><td rowspan=1 colspan=1>adKI</td><td rowspan=1 colspan=1>(4) up8uaT</td><td rowspan=1 colspan=1>() uP!M</td></tr><tr><td rowspan=1 colspan=1>A</td><td rowspan=1 colspan=1>B</td><td rowspan=1 colspan=1>D</td><td rowspan=1 colspan=1>OL</td><td rowspan=1 colspan=1>H</td><td rowspan=1 colspan=1>RD</td><td rowspan=1 colspan=1>E</td><td rowspan=1 colspan=1>F</td><td rowspan=1 colspan=1>TR</td><td rowspan=1 colspan=1>I</td><td rowspan=1 colspan=1>J</td><td rowspan=1 colspan=1>K</td><td rowspan=1 colspan=1>L</td><td rowspan=1 colspan=1>UCL</td><td rowspan=1 colspan=1>UCW</td><td rowspan=1 colspan=1>M</td><td rowspan=1 colspan=1>N</td></tr><tr><td rowspan=1 colspan=1>S-55/H19</td><td rowspan=1 colspan=1>7,900</td><td rowspan=1 colspan=1>62.6</td><td rowspan=1 colspan=1>62.6</td><td rowspan=1 colspan=1>13.1</td><td rowspan=1 colspan=1>53</td><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>1-T</td><td rowspan=1 colspan=1>2&amp;12</td></tr><tr><td rowspan=1 colspan=1>S-58/H34</td><td rowspan=1 colspan=1>14,600</td><td rowspan=1 colspan=1>65.8</td><td rowspan=1 colspan=1>65.8</td><td rowspan=1 colspan=1>15.9</td><td rowspan=1 colspan=1>56</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>11.4</td><td rowspan=1 colspan=1>38</td><td rowspan=1 colspan=1>9.5</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>6.4</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>28.3</td><td rowspan=1 colspan=1>14</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;16</td></tr><tr><td rowspan=1 colspan=1>S-61/H-3</td><td rowspan=1 colspan=1>22,000</td><td rowspan=1 colspan=1>72.8</td><td rowspan=1 colspan=1>72.8</td><td rowspan=1 colspan=1>19</td><td rowspan=1 colspan=1>62</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>12.3</td><td rowspan=1 colspan=1>40</td><td rowspan=1 colspan=1>10.3</td><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1>8.6</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>23.5</td><td rowspan=1 colspan=1>14</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>3&amp;28</td></tr><tr><td rowspan=1 colspan=1>S-76A/B/C/D</td><td rowspan=1 colspan=1>11,700</td><td rowspan=1 colspan=1>52.5</td><td rowspan=1 colspan=1>52.5</td><td rowspan=1 colspan=1>14.6</td><td rowspan=1 colspan=1>44</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>8.2</td><td rowspan=1 colspan=1>30.5</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>6.5</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>16.4</td><td rowspan=1 colspan=1>8</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;12</td></tr><tr><td rowspan=1 colspan=1>S-92</td><td rowspan=1 colspan=1>26,500</td><td rowspan=1 colspan=1>68.5</td><td rowspan=1 colspan=1>68.5</td><td rowspan=1 colspan=1>17.9</td><td rowspan=1 colspan=1>56.3</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.8</td><td rowspan=1 colspan=1>39.9</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>6.9</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>20.3</td><td rowspan=1 colspan=1>10.4</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>2&amp;19</td></tr><tr><td rowspan=1 colspan=1>S-70i/UH-60LBlackhawk</td><td rowspan=1 colspan=1>22,000</td><td rowspan=1 colspan=1>64.8</td><td rowspan=1 colspan=1>64.8</td><td rowspan=1 colspan=1>16.8</td><td rowspan=1 colspan=1>53.8</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>7.7</td><td rowspan=1 colspan=1>38</td><td rowspan=1 colspan=1>11</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>6.6</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>29</td><td rowspan=1 colspan=1>9.7</td><td rowspan=1 colspan=1>2-T</td><td rowspan=1 colspan=1>3&amp;12</td></tr><tr><td rowspan=1 colspan=1>CH-53K</td><td rowspan=1 colspan=1>74,000</td><td rowspan=1 colspan=1>99.5</td><td rowspan=1 colspan=1>99.5</td><td rowspan=1 colspan=1>27.8</td><td rowspan=1 colspan=1>79</td><td rowspan=1 colspan=1>7</td><td rowspan=1 colspan=1>17</td><td rowspan=1 colspan=1>59.6</td><td rowspan=1 colspan=1>20</td><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1>9.5</td><td rowspan=1 colspan=1>wheel</td><td rowspan=1 colspan=1>27.3</td><td rowspan=1 colspan=1>13</td><td rowspan=1 colspan=1>3-T</td><td rowspan=1 colspan=1>3&amp;55</td></tr></table>

## APPENDIX D. DIMENSIONS FOR MARKING SIZE AND WEIGHT LIMITATIONS

The form and proportion of numbers and letters for marking TLOF and parking area size and weight limitations are shown in the two figures below for both 36-inch (0.9 m) and 18-inch (0.5 m) numbers.

Figure D-1. Form and Proportions of 36-inch (0.9 m) Numbers for Marking Size and Weight Limitations  
![ec8662935c10d8dee0df5838a714f8f65d85aebc31300de8cdd317aca81d2f22.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ec8662935c10d8dee0df5838a714f8f65d85aebc31300de8cdd317aca81d2f22.jpg)

Figure D-2. Form and Proportions of 18-inch (0.5 m) Numbers for Marking Size and Weight Limitation  
![2b6a9a52e1680e2bbae00edb48d7d406d03d0df4fed62ce67c2fa20bdfebf426.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2b6a9a52e1680e2bbae00edb48d7d406d03d0df4fed62ce67c2fa20bdfebf426.jpg)

## Page Intentionally Blank

## APPENDIX E. ASSOCIATED PUBLICATIONS AND RESOURCES

The following is a listing of related documents and resources:

E.1 Current Electronic Code of Federal Regulations (e-CFRs) are available from the Government Printing Office website https://www.ecfr.gov/.

14 CFR Part 27 Airworthiness Standards: Normal Category Rotorcraft

14 CFR Part 29 Airworthiness Standards: Transport Category Rotorcraft

14 CFR Part 77 Safe, Efficient Use, and Preservation of the Navigable Airspace

14 CFR Part 91 General Operating and Flight Rules

14 CFR Part 121 Air Carrier Certification

14 CFR Part 135 Operating Requirements: Commuter and on demand operations and rules governing persons on board such aircraft

14 CFR Part 139 Certification of Airports

14 CFR Part 151 Federal Aid to Airports

14 CFR Part 152 Airport Aid Program

14 CFR Part 157 Notice of Construction, Alteration, Activation, and Deactivation of Airports

29 CFR Part 1910 Occupational Safety and Health Standards

29 CFR Part 1926 Safety and Health Regulations for Construction

E.2 Airport Advisory Circulars are available at the Airports website https://faa.gov/airports/resources/advisory\_circulars/.

AC 70/7460-1 Obstruction Marking and Lighting

AC 150/5020-1 Noise Control and Compatibility Planning for Airports

AC 150/5190-4 A Model Zoning Ordinance to Limit Height of Objects Around Airports

AC 150/5200-30 Airport Field Condition Assessments and Winter Operations Safety

AC 150/5210-5 Painting, Marking, and Lighting of Vehicles Used on an Airport

AC 150/5220-16 Automated Weather Observing Systems (AWOS) for Non-Federal Applications

AC 150/5230-4 Aircraft Fuel Storage, Handling, and Dispensing on Airports

AC 150/5320-6 Airport Pavement Design and Evaluation

AC 150/5340-30 Design and Installation Details for Airport Visual Aids

AC 150/5345-12 Specification for Airport and Heliport Beacons

AC 150/5345-27 Specification for Wind Cone Assemblies

AC 150/5345-28 Precision Approach Path Indicator Systems (PAPI)

AC 150/5345-39 FAA Specification L-853, Runway and Taxiway Retroreflective Markers

AC 150/5345-42 Specification for Airport Light Bases, Transformer Housings, Junction Boxes, and Accessories

AC 150/5345-46 Specification for Runway and Taxiway Light Fixtures

AC 150/5345-52 Generic Visual Glideslope Indicators (GVGI)

AC 150/5360-13 Airport Terminal Planning

AC 150/5360-14 Access to Airports by Individuals with Disabilities

AC 150/5370-10 Standards for Specifying Construction of Airports

E.3 Technical reports are available at the National Technical Information Service (NTIS) website https://www.ntis.gov/.

FAA/RD-84/25 Evaluating Wind Flow Around Buildings on Heliport Placement, National Technical Information Service (NTIS) accession number AD-A153512

FAA/RD-92/15 Potential Hazards of Magnetic Resonance Imagers to Emergency Medical Service Helicopter Services, National Technical Information Service (NTIS) accession number AD-A278877

Roadmap for Performance Based Navigation (PBN)

E.4 FAA 8260-series Orders, various on flight procedures, airspace, and others.

FAA Order 8260.3 U.S. Standard for Terminal Instrument Procedures (TERPS)

FAA Order 8260.54 U.S. Standard for Area Navigation (RNAV)

FAA Order 8260.58 U.S. Standard for Performance Based Navigation (PBN)

FAA Order 1050.1 Environmental Impacts: Policies and Procedures

FAA Order 5050.4 National Environmental Policy Act (NEPA) Implementing Instructions for Airport Actions

FAA Order JO 7400.2 Procedures for Handling Airspace Matters

E.5 FAA Engineering Briefs (EBs). Engineering Brief #67 Light Sources Other Than Incandescent and Xenon for Airport and Obstruction Lighting Fixtures

E.6 To find state and regional aviation offices, see https://www.faa.gov/airports/resources/state\_aviation/.

E.7 For information about grant assurances, see https:/www.faa.gov/airports/aip/grant\_assurances.

FAA Grant Assurance No. 34, Policies, Standards, and Specifications

FAA Passenger Facility Charge (PFC) Assurance No. 9, Standards and Specifications

E.8 International Civil Aviation Organization (ICAO). ICAO Annex 14, Vol. II Heliports

E.9 International Codes. International Building Code International Fire Code

E.10 National Fire Protection Association (NFPA).

NFPA 10 Standard for Portable Fire Extinguishers

NFPA 407 Standard for Aircraft Fuel Servicing

NFPA 409 Standard on Aircraft Hangars

NFPA 418 Standard for Heliports

NFPA 460 Standard for Aircraft Rescue and Fire-Fighting Services at Airports

E.11 Society of Automotive Engineers (SAE). SAE 25050 Colors, Aeronautical Lights and Lighting Equipment, General Requirements For

## Page Intentionally Blank

## APPENDIX F. HELIPORT EVALUATION PROCESS FLOW CHART

![d49c9ff28d0c6fa29a27d1ff8be2a5413c39665ee9378ed95c3edce2a743e4a7.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d49c9ff28d0c6fa29a27d1ff8be2a5413c39665ee9378ed95c3edce2a743e4a7.jpg)

## Page Intentionally Blank

## APPENDIX G. DESIGN REQUIREMENTS FOR HELIPORT PERIMETER LIGHTING

## G.1 Elevated and In-pavement Omnidirectional Helipad Perimeter Light.

## G.1.1 Horizontal Beam Coverage.

Approaches to heliports are typically performed into the prevailing wind direction. Helicopters can approach the heliport from any direction. Ensure the intensity for heliport perimeter lighting is maintained for all possible directions of approach, requiring an omnidirectional horizontal light geometry.

## G.1.2 Vertical Beam Coverage.

The approach paths flown by the helicopter pilot dictate the required vertical intensity coverage of the light fixture. The FAA Flight Standards Service determined the vertical approach paths used by most helicopters making approaches to a heliport in VMC due to limited availability of accurate data. See Table G-1.

Table G-1. Helicopter Approach Angles Assuming VMC
<table><tr><td rowspan=1 colspan=1>Approach</td><td rowspan=1 colspan=1>Typical Descent Angle</td></tr><tr><td rowspan=1 colspan=1>Shallow</td><td rowspan=1 colspan=1>3 degrees to 5 degrees</td></tr><tr><td rowspan=1 colspan=1>Normal</td><td rowspan=1 colspan=1>7 degrees to 12 degrees</td></tr><tr><td rowspan=1 colspan=1>Steep</td><td rowspan=1 colspan=1>12 degrees to 15 degrees</td></tr></table>

The approach path data were converted to the corresponding angle of elevation from the heliport perimeter lighting as a function of range. The mean angle of elevation and the upper and lower limits of the vertical beam spread will increase as the range from the heliport decreases. By controlling the vertical intensity distribution of the heliport perimeter lighting as a function of elevation, it is ensured that the lighting is sufficiently bright to be seen at the required range without glare at closer ranges.

## G.1.3 Helipad Perimeter Lighting Intensity.

The intensity requirements were developed into a specification that can be used by industry to produce and install optimized perimeter lighting. The intensity specification is based on a currently available light fixture FAA type L-860E that was determined to be the most effective in meeting the need for the pilot to be able to clearly see the perimeter lighting.

## G.1.4 Helipad Perimeter Lighting Chromaticity.

Ensure helipad perimeter light fixtures meet chromaticity requirements for aviation green per AC 150/5345-46 and SAE AS 25050, Colors, Aeronautical Lights and Lighting Equipment, General Requirements For, when using incandescent lights. For light fixtures that use light emitting diodes (LEDs) see the requirements in Engineering Brief #67.

## G.2 Photometric Requirements.

Refer to Table G-2 for the heliport perimeter light fixture photometric requirements.   
Figure G-1 illustrates the proposed light fixture intensity distribution.

Table G-2. Perimeter Lighting Intensity Recommendations
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=2>0 to 15 degrees</td><td rowspan=1 colspan=1>16 to 90 degrees</td></tr><tr><td rowspan=1 colspan=1>Color</td><td rowspan=1 colspan=1>Minimum</td><td rowspan=1 colspan=1>Minimum averageintensity</td><td rowspan=1 colspan=1>Minimum</td></tr><tr><td rowspan=1 colspan=1>Green</td><td rowspan=1 colspan=1>10</td><td rowspan=1 colspan=1>15</td><td rowspan=1 colspan=1>5</td></tr></table>

See AC 150/5345-46D, Specification/or Runway and Taxiway Light Fixtures, paragraph  
3.3, Photometric Requirements, for detailed measurement methods and requirements.

Figure G-1. Perimeter Light Intensity Distribution  
![3a52bfab21adc67ed19268490f2d014496fd0b43b4b09138e0241e9175d21d27.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3a52bfab21adc67ed19268490f2d014496fd0b43b4b09138e0241e9175d21d27.jpg)

## G.3 Additional Heliport Perimeter Light Requirements.

The construction, materials, environmental requirements, and production testing for the qualification and acceptance of elevated helicopter perimeter light fixtures, per AC 150/5345-46.

## G.3.1 LED Light Fixtures.

The additional requirements in Engineering Brief #67 are applicable for light fixtures that use LEDs.

Some night vision goggle systems may not detect specific LED colors.

## G.3.2 Light Fixture Type Number.

The light fixtures will be listed in AC 150/5345-46 as FAA type L-860H, elevated heliport perimeter light and Type L-852H, in-pavement heliport perimeter light.

## G.3.3 Light Base Requirements.

Elevated heliport perimeter light fixtures will be installed in a load-bearing light base (L-868, Size B) or non-load-bearing light base (L-867, Size B), per AC 150/5345-42. Shallow base type light bases will not be used.

## G.4 L-860H and L-852H Light Fixture Testing.

## G.4.1 Laboratory Testing.

The prototype L-860H and L-852H light fixture will be fully characterized in the laboratory using a goniometer and calibrated photo-detector for spatial light intensity distribution. For vertical angles of 0 to 10 degrees, the light intensity will be measured for each 1 degree vertically over 360 degrees horizontally (5-degree intervals). For vertical angles of 10 to 90 degrees, visually verify the projected light intensity.

All testing requirements specified in AC 150/5345-46 will be observed except for photometric requirements.

## G.4.2 Reports.

At the conclusion of all testing, the manufacturer will generate a report that details the photometric testing results in the laboratory per paragraph G.4.1.

## G.4.3 Production.

All subsequent L-860H and L-852H light fixture production will be based upon the documented results of testing, per paragraph G.4.1.

## G.5 Installation Criteria.

Heliport light fixtures will be installed in accordance with the requirements of AC 150/5340-30.

## Advisory Circular Feedback

If you find an error in this AC, have recommendations for improving it, or have suggestions for new items/subjects to be added, you may let us know by (1) mailing this form to Manager, Airport Engineering Division, Federal Aviation Administration ATTN: AAS-100, 800 Independence Avenue SW, Washington DC 20591 or (2) faxing it to the attention of the Office of Airport Safety and Standards at (202) 267-5383.

Subject: AC 150/5390-2D

Date:

Please check all appropriate line items:

☐ An error (procedural or typographical) has been noted in paragraph on page .

☐ Recommend paragraph on page be changed as follows:

☐ In a future change to this AC, please cover the following subject: (Briefly describe what you want added.)

☐ Other comments:

☐ I would like to discuss the above. Please contact me at (phone number, email address).

Submitted by:

Date:

# FAA EB-105 Vertiports (Original 2022)

## Memorandum

Date: September 21, 2022

To: All Airports Regional Division Managers

From: Michael A.P. Meyers, P.E. Manager, Airport Engineering Division, AAS-100

![fd1c5f97e2ac0676019e6e9080ccd691f167fee24f7065f9609cdc68a9d81dff.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/fd1c5f97e2ac0676019e6e9080ccd691f167fee24f7065f9609cdc68a9d81dff.jpg)

Prepared by: Robert Bassey, P.E., AAS-110

Subject: Engineering Brief No. 105, Vertiport Design

This Engineering Brief provides interim guidance for the design of vertiports for aircraft with vertical takeoff and landing (VTOL) capabilities. Note that this interim guidance will be subject to update as data, analysis, and VTOL aircraft and operations develop in the future.

# ENGINEERING BRIEF #105

# Vertiport Design

## I Purpose.

This Engineering Brief (EB) specifies design guidance for public and private vertiports and vertistops, including modification of existing helicopter and airplane landing facilities, and establishment of new sites. While the design guidance contained herein refers to vertiport design, the design guidance applies to both vertiports and vertistops where appropriate. This EB is written for vertical takeoff and landing (VTOL) aircraft powered with electric motors and utilizing distributed electric propulsion in contrast to propulsion systems built solely around an internal combustion engine.

At this time, the Federal Aviation Administration (FAA) does not have enough validated VTOL aircraft performance data and necessarily is taking a prescriptive and conservative approach with the recommendations in this EB. Vertiport guidance is expected to evolve into a performance-based design standard, potentially with aircraft grouped by their performance characteristics. This EB is written for aircraft with a maximum takeoff weight (MTOW) of 12,500 lbs (5,670 kg) or less.

This EB is a living document that serves as the FAA’s initial interim guidance and will be updated over time to adapt and address new aircraft and technology as performance data is received. Figures in this document are general representations and are not to scale.

## II Background.

The FAA has identified a need for guidance for vertiports to be utilized by VTOL aircraft.

The FAA’s previous Advisory Circular (AC) on Vertiport Design, published on May 31, 1991, provided guidance for vertiport design and was based on civil tiltrotors modeled after military tiltrotor technology. However, the intended aircraft were never used commercially, and the AC was cancelled on July 28, 2010. Currently the closest type of aviation infrastructure, being used by many for comparison purposes, is heliports and helistops. AC 150/5390-2, Heliport Design, is based on helicopters with single, tandem (front and rear) or dual (side by side) rotors. The emerging VTOL aircraft are not proven to perform like conventional helicopters or very large tiltrotor aircraft.

This EB provides the interim guidance needed to support initial infrastructure development for VTOL operations. This EB provides guidance for existing vertiport design and geometry elements. This guidance is correlated to the reference VTOL aircraft described in paragraph 1.5 below. The Reference Aircraft represents a VTOL aircraft that integrates certain performance and design characteristics of nine emerging aircraft currently in development and is used to specify certain performance and design characteristics that informed the guidance in this EB. The Reference Aircraft was developed based on interactions with original equipment manufacturers (OEMs) and multiple FAA lines of business (LOBs).

There is currently limited demonstrated performance data on how VTOL aircraft operate. Research efforts are underway to better understand the performance capabilities and design characteristics of emerging VTOL aircraft. The FAA will develop a performancebased AC on vertiport design in the future, as additional performance data is gleaned about these emerging VTOL aircraft. The AC will detail categories of vertiport facilities requiring different design criteria depending on the characteristics of the aircraft they plan to support as well as the activity levels at the facility.

The future guidance will address more advanced operations including autonomy, different propulsion methods, density, frequency, and complexity of operations facilities. The AC on vertiport design will also address VTOL aircraft using alternative fuel sources such as hydrogen and hybrid. Future guidance will also include aircraft that do not currently conform to the Reference Aircraft included in this EB (for example, aircraft with an MTOW over 12,500 pounds (5,670 kg)) and address instrument flight rules (IFR) capability and the use of multiple final approach and takeoff areas (FATOs).

To support the development of a comprehensive vertiport design AC, additional research is required to garner VTOL aircraft performance data on downwash/outwash, failure conditions or degradation of performance, landing precision, climb/descend gradients, and all azimuth weather capabilities. The data will be collected and used by the FAA research team to fill in aircraft information gaps. This will require coordination within the FAA across the various LOBs, as well as external collaboration with manufacturers and other stakeholders. A proponent interested in sharing data must work with FAA Office of Airport Safety and Standards to provide validated empirical data that addresses these performance data gaps.

## III Application.

This EB is intended as interim guidance for vertiport design until a more comprehensive performance-based vertiport design AC is developed. The guidance herein is not legally binding in its own right and will not be relied upon by the FAA as a separate basis for affirmative enforcement action or other administrative penalty. Conformity with this guidance, as distinct from existing statutes, regulations, and grant assurances, is voluntary only, and nonconformity will not affect existing rights and obligations. The standards and guidance contained in this EB are practices the FAA recommends to establish an acceptable level of safety, performance and operation in the design of new civil vertiports, and for modifications of existing helicopter and airplane landing facilities to accommodate operations of VTOL aircraft.

The vertiport design criteria in this EB is intended for VTOL aircraft that meet the performance criteria and design characteristics of the Reference Aircraft described in paragraph 1.5 and Table 1-1, flying in visual meteorological conditions (VMC) with the pilot on board. These design recommendations are for a single aircraft using the touchdown and lift off (TLOF) area, FATO area, and Safety Area at one time. Vertiport operators working with the proponent referencing this EB are responsible for confirming the ingress and egress path is clear. See paragraph 2.5.

Table 1-1: Reference Aircraft
<table><tr><td>Design Characteristics</td><td>Criteria</td></tr><tr><td>Propulsion</td><td>Electric battery driven, utilizing distributed electric propulsion</td></tr><tr><td>Propulsive units</td><td>2 or more</td></tr><tr><td>Battery systems</td><td>2 or more</td></tr><tr><td>Maximum takeoff weight (MTOW)</td><td>12,500 pounds (5,670 kg) or less</td></tr><tr><td>Aircraft length</td><td>50 feet (15.2 m) or less</td></tr><tr><td>Aircraft width</td><td>50 feet (15.2 m) or less</td></tr><tr><td></td><td></td></tr><tr><td>Operating Conditions Operation location</td><td>Criteria Land-based (ground or elevated) – no</td></tr><tr><td></td><td>amphibian or float operations</td></tr><tr><td>Pilot Flight conditions</td><td>On board</td></tr><tr><td></td><td>VFR</td></tr><tr><td>Performance</td><td>Criteria</td></tr><tr><td>Hover</td><td>Hover out of ground effect (HOGE) in</td></tr><tr><td></td><td>normal operations</td></tr><tr><td>Takeoff Landing</td><td>Vertical Vertical</td></tr><tr><td>Downwash/Outwash</td><td>Must be considered in TLOF/FATO sizing and ingress/egress areas to ensure</td></tr><tr><td></td><td>no endangerment to people/property in the vicinity, and no impact to safety critical navigational aids and surfaces, supporting equipment, nearby aircraft, and overall safety</td></tr></table>

Further research is needed to understand VTOL taxiing and parking needs. In future guidance, parking and taxiway guidance will be included. If necessary in the interim, vertiports designed for ground taxiing can follow AC 150/5300-13, Airport Design, taxiway guidelines for Group 1 aircraft. For hover taxi, vertiport design should follow taxiway guidance in AC 150/5390-2, Heliport Design, for the Transport Category. For parking, vertiport design should follow guidance in AC 150/5390-2 for the Transport Category.

For vertiport facilities that will also accommodate helicopter operations, the proponent should follow the recommendations in this EB and mark the facility as a vertiport unless the facility is built to the Transport Category heliport design standard, as described in paragraph 3.0.

This EB provides guidance on marking, lighting, and visual aids that identify the facility as a vertiport. This guidance applies to new vertiports or to heliports that are altered to vertiports.

Vertiport facilities that are intended to serve aircraft that do not meet the performance criteria and design characteristics of the Reference Aircraft included in this EB should begin coordination with the applicable FAA Regional or Airports District Office early in the planning and design process for the takeoff and landing area and will be subject to review on a case-by-case basis.

## V Questions.

Contact the FAA Airport Engineering Division, AAS-100, for any questions about this EB.

## VI Effective Date.

This EB becomes effective as of the date the associated memorandum is signed by the Manager, FAA Airport Engineering Division, AAS-100.

## Table of Contents

1.0 Introduction...... ............................................... 8   
1.1. Engineering Brief (EB) Guideline Justification.. ...................... ..... 8   
1.2. Explanation of Terms...... .................................................. 9   
1.3. Airspace Approval Process and Coordination. ..................................................... 11   
1.4. State/Local Role... .............................. ..... 12   
1.5. Reference Aircraft... .... 12   
2.0 Vertiport Design and Geometry. ............................................................................ ...... 14   
2.1. Overview..... .............................................................................. ..... 14   
2.2. TLOF Guidance. ... ........................................................................... .... 15   
2.3. FATO Guidance....... ........................................................................................... 17   
2.4. Safety Area Guidance. ................................................................................. ........ 19   
2.5. VFR Approach/Departure Guidance.............................................................. ..... 20   
3.0 Marking, Lighting, and Visual Aids..................................................................... ....... 24   
3.1. General... ..... 24   
3.2. Identification Symbol.. .... 26   
3.3. TLOF Size/Weight Limitation Box. ... 27   
3.4. Flight Path Alignment Optional Marking and Lighting. .................... ...... 31   
3.5. Lighting. .... … ...... 33   
3.6. Identification Beacon. . ................................ ...... 40   
3.7. Wind Cone. .. ..... 40   
4.0 Charging and Electric Infrastructure......... ...... 41   
4.1. Standards.. ..... 41   
5.0 On-Airport Vertiports. . .... 44   
5.1. On-Airport Location of TLOF. . ... 44   
5.2. On-Airport Location of FATO... .... 44   
6.0 Site Safety Elements....... ............................................................................ 46   
6.1. Fire Fighting Considerations... .......................................... .... 46   
6.2. Security and Safety. ...................................................................................... ........ 46   
6.3. Downwash/Outwash. . ..................................................................... ....... 48   
6.4. Turbulence. ... ............ ..... 48   
6.5. Weather Information.. ... 49   
6.6. Winter Operations. .. ... 49   
6.7. Access to Vertiports by Individuals with Disabilities... .. 49   
Acronym List.. . 50

## Figures

Figure 2-1: Relationship and Dimensions of TLOF, FATO, and Safety Area . . 14   
Figure 2-2: Vertiport Gradients and Rapid Runoff Shoulder . . 17   
Figure 2-3: VFR Vertiport Approach/Departure Surfaces.. .... 22   
Figure 3-1: Standard Vertiport Marking . .. 25   
Figure 3-2: Vertiport Identification Symbol . ... 26   
Figure 3-3: TLOF Size/Weight Limitation Box .. 28   
Figure 3-4: Form and Proportions of 36-inch (914 mm) Numbers for Marking Size and Weight   
Limitations .. ... 29   
Figure 3-5: Form and Proportions of 18-inch (457 mm) Numbers for Marking Size and Weight   
Limitations .. .... 30   
Figure 3-6: Flight Path Alignment Marking and Lighting.. .. 32   
Figure 3-7: TLOF/FATO Perimeter Lighting.... ... 36   
Figure 3-8: Elevated Vertiport Configuration Example . ... 37   
Figure 3-9: Elevated FATO Perimeter Lighting. ... 38   
Figure 5-1: Example of an On-airport Vertiport. . 45   
Figure 6-1: Vertiport Caution Sign .... . 48

## Tables

Table 1-1: Reference Aircraft . . 4   
Table 2-1: Takeoff and Landing Area Dimensions . . 14   
Table 3-1: Perimeter Lighting Intensity and Distribution. . 34   
Table 5-1: Recommended Minimum Distance between Vertiport FATO Center to Runway   
Centerline for VFR Operations.. . 45

## 1.0 Introduction.

## 1.1. Engineering Brief (EB) Guideline Justification.

Information collected through a literature review and original equipment manufacturer (OEM) coordination indicates that emerging VTOL aircraft will demonstrate similar performance characteristics to helicopters. However, limited data is available on VTOL aircraft operational characteristics, performance, maneuverability, downwash/outwash impacts, and vertiport obstacle information needs. Consequently, this EB is limited to pilot-on-board, visual flight rule (VFR) operations, and VTOL aircraft that have the characteristics and performance of the Reference Aircraft described in paragraph 1.5.

Heliports provide the most analogous present-day model for vertiports. However, despite the similarities between the two types of aircraft, there are design differences between traditional helicopters and VTOL aircraft. VTOL aircraft have varied configurations and propulsion systems, with and without wings, and with varied landing configurations. As a result, the conversion ratio in AC 150/5390-2 of 0.83  the overall length being used to calculate the main rotor diameter of the design helicopter is not representative of the diverse characteristics associated with the various VTOL aircraft being developed. In addition, there persists a lack of validated data on the performance capabilities of VTOL aircraft.

The limited tangible data available to validate OEM performance, especially in failure conditions, recommends a wider touchdown and liftoff area (TLOF) and load bearing final approach and takeoff area (FATO) than currently required for a general aviation heliport in AC 150/5390-2. Due to these performance data gaps, including downwash, the larger physical dimensions would accommodate a potentially wider landing scatter and decreased climb performance in different scenarios

The anticipated Advanced Air Mobility (AAM) density, frequency, and complexity of operations is expected to be high in some cases. These operations are also anticipated to include commercial and air carrier operators, and will require certain safety levels and infrastructure requirements most analogous to the predetermined level of safety set in the Transport Category heliport design guidelines in AC 150/5390-2.

Preliminary data garnered from the VTOL aircraft manufacturers to support the development of this EB claims no need by the aircraft for effective transitional lift (ETL) to fly and an ability to hover out of ground effect (HOGE). Therefore, the minimum sizing standards that accommodate the need for ETL per the Transport Category heliport criteria (e.g., 100 feet (30.5 m) by 200 feet (61 m) FATO) is not specified in this EB. As such, this EB is intended for aircraft that have HOGE capability. If the vertiport design VTOL aircraft is proven not to perform HOGE, this EB is not applicable, and the sponsor must work directly with the FAA to determine alternative vertiport sizing for that design VTOL aircraft.

## 1.2. Explanation of Terms.

Terms used in this EB:

1. Approach/Departure Path: The approach/departure path is the flight track that VTOL aircraft follow when landing at or taking off from a vertiport.

2. Battery: One or more electrically connected cells, assembled in a single container having positive and negative terminals. A battery may include inter-cell connectors and other devices.

3. Battery pack: Two or more battery systems.

4. Battery system: Comprised of the battery, the battery charger and any protective, monitoring, and alerting circuitry or hardware inside or outside of the battery. It also includes vents (where necessary) and packaging.

5. Controlling dimension (D): The diameter of the smallest circle enclosing the VTOL aircraft projection on a horizontal plane, while the aircraft is in the takeoff or landing configuration, with rotors/propellers turning, if applicable. See Figure 1-1.

6. Design VTOL aircraft: The design VTOL aircraft is the largest electric, hydrogen, or hybrid VTOL aircraft that is expected to operate at a vertiport. This design VTOL aircraft is used to size the TLOF, FATO and Safety Area. Note that the design VTOL aircraft is different from the Reference Aircraft used to define the performance and design criteria in this EB.

7. Downwash/Outwash: The downward and outward movement of air caused by the action of rotating rotor blade, propeller, or ducted fan. When this air strikes the ground or some other surface, it causes a turbulent outflow of air from the aircraft.

8. Elevated vertiport: A vertiport is considered elevated if it is located on a rooftop or other elevated structure where the TLOF and FATO are at least 30 inches (0.8 m) above the surrounding surface (a ground level vertiport with the TLOF on a mound is not an elevated vertiport).

9. Effective transitional lift (ETL): The pronounced increase in translational lift during transition to forward flight due to the rotor/propeller experiencing a significantly decreased induced airflow.

10. Failure condition (FC): FC is generally defined as an occurrence of any likely event, caused or contributed to by one or more failures, which affects the aircraft’s ability to generate lift or thrust and results in a consequential state that has an impact for a given flight phase.

Figure 1-1: Controlling Dimension  
![a6d05565df2eea5515444710f033b3d3f83f009319ebd2b0da1ebd1b1fac380e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a6d05565df2eea5515444710f033b3d3f83f009319ebd2b0da1ebd1b1fac380e.jpg)

11. Final approach and takeoff area (FATO): The FATO is a defined, load-bearing area over which the aircraft completes the final phase of the approach, to a hover or a landing, and from which the aircraft initiates takeoff.

12. Ground Effect: A condition of usually improved performance encountered when the aircraft is operating very close to the ground or a surface. It results from a reduction in upwash, downwash, and/or blade tip vortices, which provide a corresponding decrease in induced drag.

13. Hover: The word “hover” applies to an aircraft that is airborne and remaining in one place at a given altitude over a fixed geographical point regardless of wind. Pure hover is accomplished only in still air. For the purpose of this EB, the word “hover” will mean pure hover.

14. Hover out of ground effect (HOGE): The ability to achieve hover without the benefit of the ground or a surface.

15. Imaginary surface(s): The imaginary planes defined in Title 14 Code of Federal Regulations (CFR) Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, centered about the FATO and the approach/departure paths, which are used to identify the objects where notice to and evaluation by the FAA is required.

16. Obstruction to air navigation: Any fixed or mobile object, including a parked aircraft, of greater height than any of the heights or surfaces presented in subpart C of 14 CFR Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace.

17. Reference Aircraft: The Reference Aircraft represents a VTOL aircraft that integrates certain performance and design characteristics of nine emerging aircraft currently in development. This Reference Aircraft is used to specify certain performance and design characteristics that informed the vertiport design guidance in this EB.

18. Safety Area: The Safety Area is a defined area surrounding the FATO intended to reduce the risk of damage to aircraft accidentally diverging from the FATO.

19. Translational Lift: Translational lift is the improved rotor/propeller efficiency resulting from directional flight.

20. Touchdown and liftoff area (TLOF): The TLOF is a load bearing, generally paved area centered in the FATO, on which the aircraft performs a touchdown or liftoff.

21. Vertiport: An area of land, or a structure, used or intended to be used, for electric, hydrogen, and hybrid VTOL aircraft landings and takeoffs and includes associated buildings and facilities.

22. Vertiport elevation: The highest elevation of all usable TLOFs within the vertiport expressed in feet above mean sea level (MSL).

23. Vertistop: A vertistop is a term generally used to describe a minimally developed vertiport for boarding and discharging passengers and cargo (i.e., no fueling, defueling, maintenance, repairs, or storage of aircraft, etc.). The design standards and recommendations in this EB apply to all vertiports, which includes vertistops.

## 1.3. Airspace Approval Process and Coordination.

For vertiport development on federally obligated airports, the infrastructure or equipment must be depicted on the Airport Layout Plan (ALP) and a Form 7460-1 submitted for an airspace determination prior to development. The FAA’s review of the ALP and airspace determination must be completed prior to the start of operations.

For development on non-federally obligated airports or heliports or for non-federally funded standalone vertiport sites, and in compliance with 14 CFR Part 157, Notice of Construction, Alteration, Activation, and Deactivation of Airports, the proponent must submit FAA Form 7480-1, Notice for Construction, Alteration and Deactivation of Airports, at least 90 days in advance of the day that construction work is to begin on the takeoff and landing area. Note: Airspace determination is not tied to this 90-day advance notice. Given the nascence of the AAM industry, the FAA highly encourages that engagement with the appropriate FAA regional or district office begin before the submission of the Form 7480-1, but an FAA evaluation is predicated on the submitted Form 7480-1.

Heliport facilities that are being altered in geometry in accordance with the design criteria in this EB, if non-federally funded, the sponsor will need to submit a new Form 7480-1 to re-designate the facility as a vertiport before VTOL operations should commence at the site. The Form 7480-1 can be submitted electronically as a Landing Area Proposal (LAP) at OEAAA.faa.gov. The FAA’s Flight Standards Service Office will determine when to do an onsite evaluation using risk-based analysis.

## 1.4. State/Local Role.

Many state departments of transportation, aeronautics commissions, or similar authorities require prior approval and, in some instances, a license or permit to establish and operate landing facilities. Those seeking to establish a vertiport should first contact their respective state or local transportation or aeronautics departments or commissions for specifics on applicable licensing or permitting. Several states and municipalities also administer a financial assistance program like the federal program and are staffed to provide technical advice. Contact information for state aviation agencies is available at https://www.faa.gov/airports/resources/state\_aviation/.

In addition to state requirements, many local communities have enacted zoning ordinances, building and fire codes, and conditional use permitting requirements that can affect the establishment and operation of landing facilities. Some communities have developed codes or ordinances regulating environmental issues such as noise and air pollution. Therefore, communities, proponents, or sponsors seeking to establish a publicor private-use vertiport should make early contact with:

 local officials or agencies representing the local zoning board;

 the fire, police, or sheriff's department; and

 stakeholders who represent the area where the vertiport is to be located.

State regulators, departments of transportation, and local communities can also use the guidance and best practices outlined in this EB when reviewing a proposed vertiport facility or developing independent standards.

In addition to state and local coordination, vertiport proponents are encouraged to coordinate potential sites with any nearby airports or aviation stakeholders. Lack of early coordination can cause airspace, operational, safety, capacity, and financial impacts. While the FAA will review all new vertiport proposals for the safe and efficient utilization of navigable airspace by aircraft and the safety of persons and property on the ground, early coordination with these entities may offer early insights into airspace and capacity conflicts before investments are made.

## 1.5. Reference Aircraft.

The Reference Aircraft represents a VTOL aircraft that integrates certain performance and design features of nine emerging aircraft currently in development. This Reference Aircraft is used to specify the performance and design characteristics for the purposes of vertiport design in this EB.

Emerging VTOL aircraft models are evolving rapidly with OEMs approaching aircraft certification from a wide range of different designs. While aircraft classifications are useful in takeoff and landing area design and airspace analysis, new VTOL aircraft concepts vary significantly in terms of design, aircraft dimensions, performance, and operational characteristics. Furthermore, these new VTOL aircraft do not have an established safety record and have not yet received FAA airworthiness certification. This makes it impractical to categorize VTOL aircraft as the FAA has traditionally done with FAA certificated fixed wing and rotor aircraft. However, OEM engagement has revealed some common characteristics among VTOL aircraft prototypes including multiple propulsion systems, HOGE capability, and helicopter performance similarities.

The vertiport design guidance in this EB relies on design characteristics, expected performance capabilities, and preliminary assumptions regarding takeoff and landing area design until there is adequate research on these emerging aircraft to develop a performance-based vertiport design AC. Accordingly, the aircraft features and performance capabilities listed in Table 1-1 create a Reference Aircraft type to inform this EB. The design characteristics, performance, and operating conditions that make up this reference VTOL aircraft will be reviewed in the future as the FAA continues to engage with emerging VTOL aircraft manufacturers.

## 2.0 Vertiport Design and Geometry.

## 2.1. Overview.

The takeoff and landing area design and geometry contained in this EB includes the TLOF, the FATO, and the Safety Area. The dimensions for these areas are presented in Table 2-1 and are based on the controlling dimension (D) of the design VTOL aircraft as defined for each vertiport facility. The D is the diameter of the smallest circle enclosing the VTOL aircraft projection on a horizontal plane, while the aircraft is in the takeoff or landing configuration, with rotors/propellers turning, if applicable. See Figure 1-1. 1D is equal to the longest distance described above. The following sections provide specific details about these areas. See Figure 2-1 for the relationship among the TLOF, FATO, and Safety Area.

Table 2-1: Takeoff and Landing Area Dimensions
<table><tr><td rowspan=1 colspan=1>Element</td><td rowspan=1 colspan=1>Dimension</td></tr><tr><td rowspan=1 colspan=1>TLOF</td><td rowspan=1 colspan=1>1D</td></tr><tr><td rowspan=1 colspan=1>FATO</td><td rowspan=1 colspan=1>2D</td></tr><tr><td rowspan=1 colspan=1>Safety Area</td><td rowspan=1 colspan=1>3D (½ D added to edge of FATO)</td></tr></table>

Figure 2-1: Relationship and Dimensions of TLOF, FATO, and Safety Area  
![1ca421c613cda5aa62bd1905ef1defb082547b175dc222b9b3f73b4ec8f5a1a9.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/1ca421c613cda5aa62bd1905ef1defb082547b175dc222b9b3f73b4ec8f5a1a9.jpg)  
Note: As empirical validated performance data for individual VTOL aircraft is analyzed and understood, this criteria may be adjusted appropriately.

## 2.2. TLOF Guidance.

The TLOF is a load bearing, generally paved area centered in the FATO, on which the VTOL aircraft performs a touchdown or liftoff. The following guidelines apply to the TLOF:

1. Located at ground level, on elevated structures\*, or at rooftop level.

2. On level terrain or a level structure.

3. Clear of penetrations and obstructions to the approach/departure and transitional surfaces.

4. Load bearing (static and dynamic for design VTOL aircraft).

a. Supports the weight of the design VTOL aircraft and/or any ground support vehicles, whichever is more demanding for pavement design. The static loads are equal to the aircraft’s maximum takeoff weight applied through the total contact area of the landing gear.

b. Supports the dynamic loads based on 150 percent of the maximum takeoff weight of the design VTOL aircraft. For design purposes, assume the dynamic load at 150 percent of the maximum takeoff weight applied over the whole landing gear for a landing gear with wheels, and at the single point of contact for a landing gear with skids.

c. Accounts for rotor/propeller downwash load in load-bearing capacity.

5. Centered within its own FATO.

6. Minimum width is 1D†.

7. For a circular TLOF, minimum diameter is 1D.

8. Minimum length is 1D§.

9. Circular, square, or rectangular in shape‡. The TLOF should have the same shape as the FATO and Safety Area.

10. Design the distance between the TLOF, FATO and Safety Area perimeters to be equidistant regardless of the shape of the TLOF.

11. Meets general surface characteristics and pavement guidelines including the following:

a. Has a paved or aggregate-turf surface (see AC 150/5370-10, Standard Specifications for Construction of Airports, items P-217, Aggregate-Turf Runway/Taxiway, and P-501, Cement Concrete Pavement).

b. Uses cement concrete pavement when feasible. An asphalt surface is discouraged as it is susceptible to heat stress and may rut under the weight of a parked VTOL aircraft, creating loose debris and potential catch points for landing gear.

c. Has a roughened pavement finish (e.g., brushed or broomed concrete) to provide a skid-resistant surface for VTOL aircraft and a non-slippery footing for people.

d. Elevations between any paved and unpaved portions of the TLOF and FATO are equal.

e. Surface is stabilized to prevent erosion or damage from rotor/propeller downwash or outwash from VTOL aircraft operations. (Find guidance on pavement design and soil stabilization in AC 150/5320-6, Airport Pavement Design and Evaluation, and AC 150/5370-10.)

f. Preferred surface of elevated TLOFs is concrete or metal. If the surface is conductive, it may need to be insulated and/or grounded to the extent feasible to eliminate the threat of conducting electricity in cases of a short circuit or lightning strike. If the surface is metal, it should be grounded. Insulation is permissible if grounding is not feasible. Construct rooftop and other elevated TLOFs of metal, concrete, or other materials subject to local building codes.

g. Elevated TLOFs comply with 29 CFR Section 1926.34, Means of Egress, and 29 CFR Section1910.25, Stairways, as applicable.

12. Gradient provides positive drainage (between -0.5 and -1.0 percent) off of and away from the pavement as shown in Figure 2-2.

13. For rooftop or other elevated TLOFs, ensure that:

a. The FATO and TLOF are at or above the elevation of the adjacent Safety Area.

b. Elevator penthouses, cooling towers, exhaust vents, fresh-air vents, and other elevated features or structures do not affect VTOL aircraft operations or penetrate the TLOF, FATO, Safety Area, Approach Surface, or Transition Surface.

c. Fresh air vents for any attached building are not impacted by landing facility operations.

d. See paragraph 6.4, Turbulence.

Figure 2-2: Vertiport Gradients and Rapid Runoff Shoulder  
![0cbb31060bdcf748a6519950e06dc458d14bd3b4a6c09755e64818d72be9e6bf.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0cbb31060bdcf748a6519950e06dc458d14bd3b4a6c09755e64818d72be9e6bf.jpg)  
Note 1: The slope direction is based on the topography of the site.

Note 2: Grade the TLOF, FATO, and Safety Area to provide positive drainage of the entire area for the TLOF, FATO, and Safety Area.

Note 3: 2:1 maximum Safety Area gradient for vertiports at ground level or where applicable at elevated structures.

## 2.3. FATO Guidance.

The FATO is a defined area over which the VTOL aircraft completes the final phase of the approach to a hover or a landing and from which the aircraft initiates takeoff. The following guidelines apply to the FATO:

1. Located at ground level, on elevated structures, or at rooftop level.

2. Clear with no penetrations or obstructions except for navigational aids that are fixed-by-function (e.g., flight path alignment marking and lighting, approach lighting, TLOF lights)§, which must be on frangible mounts.

Note: While there is no accepted standard for frangibility regarding VTOL operations, remove all objects from a FATO and Safety Area except those of the lowest mass practicable and frangibly mounted objects no higher than 2 inches (51 mm) above the adjacent TLOF elevation, to the extent practicable.

3. Load bearing (static and dynamic for design VTOL aircraft), including the following features:

a. Supports the weight of the design VTOL aircraft and any ground support vehicles. The static loads are to be equal to the aircraft’s maximum takeoff weight applied through the total contact area of the landing gear.

b. Assume dynamic loads at 150 percent of the maximum takeoff weight of the design VTOL aircraft.

c. Rotor/propeller downwash load is accounted for in load-bearing capacity.

4. Centered within its own Safety Area.

5. Minimum width is 2D.

6. Minimum length is 2D.

7. For a circular FATO, minimum diameter is 2D.

8. The same geometric shape as the $\mathrm { T L O F } ^ { * * }$ and Safety Area.

9. Design the distance between the TLOF, FATO and Safety Area perimeters to be equidistant regardless of the shape of the TLOF.

10. Meets general surface characteristics and pavement guidelines including the following:

a. Paved or aggregate-turf surface (see AC 150/5370-10, items P-217, Aggregate-Turf Pavement and P-501, Cement Concrete Pavement).

b. Uses cement concrete pavement when feasible. An asphalt surface is less desirable as it may rut under the weight of a parked VTOL aircraft.

c. Has a roughened pavement finish (e.g., brushed or broomed concrete) to provide a skid-resistant surface for VTOL aircraft and a non-slippery footing for people.

d. Elevations between any paved and unpaved portions of the FATO are equal.

e. Surface is stabilized to prevent erosion of damage from rotor/propeller downwash or outwash from VTOL aircraft operations. (Find guidance on pavement design and soil stabilization in AC 150/5320-6 and AC 150/5370-10.)

f. Preferred surface of elevated FATO is concrete. If the surface is metal, it must be insulated/grounded to the extent feasible to eliminate the threat of conducting electricity in the case of a short circuit or lightning strike.

g. Elevated FATOs should be metal or concrete and comply with 29 CFR Section 1926.34 and 29 CFR Section1910.25, as applicable.

11. The FATO surface prevents loose stones and any other flying debris caused by rotor/propeller downwash or outwash.

12. Gradient provides positive drainage (between 1.5 and 5.0 percent) off of and away from the pavement, with a minimum 10-foot wide (3 m wide) rapid runoff shoulder sloped between 3.0 and 5.0 percent, as shown in Figure 2-2. Design a negative gradient of not more than 2 percent in any areas where a VTOL is expected to land.

13. The edge of the FATO abutting the TLOF is the same elevation as the TLOF.

14. If the FATO is located on a rooftop or other elevated structures:

a. The FATO and TLOF elevations are at or above the elevation of the adjacent Safety Areas.

b. The FATO is above the level of any obstacle in the Safety Area that cannot be removed.

c. Title 29 CFR Section 1910.28, Duty to Have Fall Protection and Falling Object Protection, requires the provision of fall protection if the platform is elevated 4 feet (1.2 m) or more above its surroundings. The FAA recommends such protection for all platforms elevated 30 inches (0.8 m) or more.

d. Does not use permanent railings or fences that would be safety hazards during aircraft operations.

e. Optionally, can use safety nets that meet state and local regulations, are at least 5 feet (1.5 m) wide, and meet the following criteria:

i. The insides and outside edges of the nets are fastened to a solid structure.

ii. The net is constructed of materials that are resistant to environmental effects and is inspected annually for integrity.

iii. The net has a load carrying capability of 50 pounds per square foot (244 kg/sq m).

iv. The net is located at or below the edge elevation of the FATO.

v. The net is attached to the outer perimeter frame of the FATO.

## 2.4. Safety Area Guidance.

The Safety Area is a defined area surrounding the FATO intended to reduce the risk of damage to VTOL aircraft unintentionally diverging from the FATO. The following guidelines apply to the Safety Area:

1. Located at ground level, on elevated structures, at rooftop level, and can extend over water or in clear airspace.

2. Clear with no penetrations or obstructions except for navigational aids that are fixed-by-function††, which must be on frangible mounts. Note: See paragraph 2.3.

3. For elevated TLOFs, no fixed objects within the Safety Area project above the FATO except those fixed-by-function which must be on frangible mounts. Note: See paragraph 2.3.

4. Minimum width is ½ D from the edge of the FATO.

5. Minimum length is ½ D from the edge of the FATO.

6. The same geometric shape as the TLOF and FATO.

7. Design the distance between the TLOF, FATO and Safety Area perimeters to be equidistant regardless of the shape of the TLOF.

8. If at ground level, the surface prevents loose stones and any other flying debris caused by downwash or outwash.

9. If at ground level, gradient provides positive drainage away from the FATO no steeper than 2:1, horizontal units and vertical units, respectively. See Figure 2-2.

10. On rooftop or other elevated FATOs, meets requirements contained in Section 1910.28.

## 2.5. VFR Approach/Departure Guidance.

## 2.5.1. VFR Approach/Departure and Transitional Surfaces.

The imaginary surfaces defined in 14 CFR Part 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, for heliports are applicable to vertiports and include the primary surface, approach, and transitional surfaces. Part 77 establishes standards and notification requirements for objects affecting navigable airspace. This notification provides the basis for:

evaluating the effect of construction or alteration on aeronautical operating procedures;

determining the potential hazardous effect of proposed construction on air navigation;

identifying mitigating measures to enhance safe air navigation; and

aeronautical charting for new objects.

The following applies to these imaginary surfaces:

1. The primary surface coincides in size and shape with the FATO. This surface is a horizontal plane at the elevation of the established vertiport elevation.

2. The approach surface (and, by reciprocal, the departure surface) begins at each end of the vertiport primary surface with the same width as the primary surface and extends outward and upward for a horizontal distance of 4,000 feet (1,219 m) where its width is 500 feet (152 m). The slope of the approach surface is 8:1, horizontal units and vertical units, respectively.

3. The transitional surfaces extend outward and upward from the lateral boundaries of the primary surface and from the approach surfaces at a slope of 2:1, horizontal units and vertical units, respectively, for 250 feet (76 m) measured horizontally from the centerline of the primary and approach surfaces.

4. The approach and transitional surfaces are clear of penetrations unless an FAA aeronautical study determines penetrations to any of these surfaces not to be hazards.

See Figure 2-3 for visual depiction of this guidance.

Figure 2-3: VFR Vertiport Approach/Departure Surfaces  
![949efb0434d5d53a9d2855aa944b3767c367e9a038061865cde4da73a9cf3cfa.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/949efb0434d5d53a9d2855aa944b3767c367e9a038061865cde4da73a9cf3cfa.jpg)  
Note 1: The preferred approach/departure surface is based on the predominant wind direction. Where a reciprocal approach/departure surface is not possible in the opposite direction, use a minimum 135-degree angle between the two surfaces.

## 2.5.2. VFR Approach/Departure Path.

The approach/departure path is the flight track that VTOL aircraft follow when landing at or taking off from a vertiport. The following guidelines apply to the approach/departure path(s):

1. Preferred approach/departure paths are aligned with the predominant wind direction as much as possible, to avoid downwind operations and keep crosswind operations to a minimum.

2. More than one approach/departure path is provided as close to reciprocal in magnetic heading as possible (e.g., 180 degrees and 360 degrees).

3. Additional approach/departure paths are based on an assessment of the prevailing winds or separated from the preferred flight path by at least but not limited to 135 degrees.

4. All approach and departure surfaces are free of obstructions.

5. The approach/departure paths must assure 8:1 horizontal units and vertical units.

6. To the extent practicable, design vertiport approach/departure paths to be independent of approaches to, and departures from, active runways if separate vertiport takeoff and landing areas are needed.

7. The approach and departure path may be curved but only the VFR approach/departure and transitional surfaces outlined in paragraph 2.5.1 are addressed in 14 CFR Part 77, Safe, Efficient Use and Preservation of the Navigable Airspace. Therefore, while they may be used, curved approaches are not evaluated by the FAA for the effect of objects (temporary or permanent, existing or new) on aeronautical operating procedures. These curved approaches are also not considered in aeronautical charting for new objects.

See Figure 2-3 for a visual depiction of this guidance.

## 3.0 Marking, Lighting, and Visual Aids.

This section provides guidance on marking, lighting, and visual aids that identify the facility as a vertiport. This guidance applies to new vertiports or to heliports that are altered to vertiports.

## 3.1. General.

The following general guidelines apply to markings:

1. Paint or preformed materials define the TLOF and FATO within the limits of those areas. See AC 150/5370-10, Item P-620, for specifications.

2. Reflective paint and retroreflective markers are optional and should be used with caution, as overuse of reflective material can be blinding to a pilot when using landing lights and/or night vision goggles.

3. Outlining markings and lines with a 2-6-inch (55-152 mm)-wide line of a contrasting color is an option to enhance conspicuousness.

4. TLOF perimeter marking is a 12-inch-wide (305 mm wide) solid white line.

5. TLOF size and weight limitation box is included on a TLOF with a hard surface (described in paragraph 3.3) and as an option on a TLOF with a turf surface.

6. FATO perimeter is marked by 12-inch-wide (305 mm wide) dashed white lines that are 5 feet (1.5 m) in length with end-to-end spacing of 5 to 6 feet (1.5 to 1.8 m) apart.

See Figure 3-1 for a visual depiction of the standard vertiport marking.

Figure 3-1: Standard Vertiport Marking  
![0c62aac0c4787b216ee4822e92a0d2ceaeec86c75b302f07e6158264336eb28d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0c62aac0c4787b216ee4822e92a0d2ceaeec86c75b302f07e6158264336eb28d.jpg)  
Figure is configured for 50-foot (15.2 m) TLOF.  
Note 1: Solid and dashed white lines are 12 inches (305 mm) in width. Dashed lines are 5-foot (1.5 m) in length with 5-6-foot (1.5-1.8 m) spaces.  
Note 2: See Figure 3-3 for details on the TLOF size/weight limitation box.

## 3.2. Identification Symbol.

The vertiport identification marking or symbol identifies the location as a vertiport, marks the TLOF, and provides visual cues to the pilot. Vertiport facilities should use the broken wheel symbol shown in Figure 3-2.‡‡ The symbol is in the center of the TLOF. Paint a 2-foot-wide (0.6 m wide) bar, of the same color as the broken wheel, 2 ft (0.6 m) below the broken wheel symbol when necessary to distinguish the preferred approach/departure direction.

Figure 3-2: Vertiport Identification Symbol  
![1a8e58202bcb2e630c121cc23359f33c29e03b20cbd803095370b17a4c209bd2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/1a8e58202bcb2e630c121cc23359f33c29e03b20cbd803095370b17a4c209bd2.jpg)  
Note 1: White lines on the vertiport identification symbol at 12 inches (305 mm) wide.  
Note 2: White bar, 10 ft  2 ft (3 m  0.6 m), denotes preferred approach/departure direction.

## 3.3. TLOF Size/Weight Limitation Box.

The TLOF size/weight limitation box indicates the controlling dimension (maximum length or width) and the maximum takeoff weight of the design VTOL aircraft that can use the vertiport. Weight limitation boxes should meet the following guidance:

1. The letter “D” and the weight, in imperial units, of the design VTOL aircraft that the vertiport is designed to accommodate are in a box in the lower right-hand corner of a rectangular TLOF, or on the right-hand side of the symbol of a circular TLOF, when viewed from the preferred approach direction.

2. The numbers are black on a white background.

3. The top number is the maximum takeoff weight of the design VTOL aircraft in thousands of pounds for the design VTOL the TLOF will accommodate. It is centered in the top half of the box.

4. The bottom number is the controlling dimension of the design VTOL aircraft, is centered in the bottom half of the box, and is preceded by the letter “D.”

5. An existing TLOF without a weight limit is marked with a diagonal line extending from the lower left-hand corner to the upper right-hand corner in the upper section of the TLOF size/weight limitation box.

See Figure 3-3 for details on the TLOF size/weight limitation box, and Figure 3-4 and Figure 3-5 for details on the form and proportions of the numbers and letters specified for these markings.

Figure 3-3: TLOF Size/Weight Limitation Box  
![f578207265209b732ffbeee4536ca687a2ccd51c2184e0dc0c445c9003d7f4f1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f578207265209b732ffbeee4536ca687a2ccd51c2184e0dc0c445c9003d7f4f1.jpg)  
Note: Make the minimum size of the box 5 ft (1.5 m) square. Where possible, increase this dimension to a 10 ft (3 m) square for improved visibility.

Figure 3-4: Form and Proportions of 36-inch (914 mm) Numbers for Marking Size and Weight Limitations  
![96aa5ed22ae89079aebeb5eae5c86e2ebd8297bf0735bcef42c3a6c8ee1c8d92.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/96aa5ed22ae89079aebeb5eae5c86e2ebd8297bf0735bcef42c3a6c8ee1c8d92.jpg)

Figure 3-5: Form and Proportions of 18-inch (457 mm) Numbers for Marking Size and Weight Limitations  
![72230cf24e44b5f70765e973bd3114b713623e21d993375038491ac3a1057bc6.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/72230cf24e44b5f70765e973bd3114b713623e21d993375038491ac3a1057bc6.jpg)

## 3.4. Flight Path Alignment Optional Marking and Lighting.

Flight path alignment marking and lighting is optional and includes markings and/or lights when it is desirable and practicable to indicate available approach and/or departure flight path direction(s). Guidance for optional flight path alignment marking and lighting includes:

1. The shaft of each arrow is 1.5 ft (0.5 m) wide and at least 10 feet (3 m) long.

2. The arrow heads are 5 feet (1.5 m) wide and 5 feet (1.5 m) tall.

3. The color of the arrow must provide good contrast against the background color of the surface. Provide a contrasting border around the arrows if needed to increase visibility for the pilot.

4. An arrow pointing toward the center of the TLOF depicts an approach direction.

5. An arrow pointing away from the center of the TLOF depicts a departure direction.

6. In-pavement flight path alignment lighting is recommended. See paragraph 3.5 for additional guidance. For elevated lights, if the TLOF light conflicts with a flight path alignment light, remove the conflicting flight path alignment light fixture.

7. For a vertiport with a flight path limited to a single approach direction or a single departure path, the arrow marking is unidirectional (i.e., one arrowhead only). For a vertiport with only a bidirectional approach/takeoff flight path available, the arrow marking is bidirectional (i.e., two arrowheads).

See Figure 3-6 for additional guidance.

Figure 3-6: Flight Path Alignment Marking and Lighting  
![a7a80ab3d4f23676806b4f3a4f648088a63faadef06729daf5fcf808523df8ee.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a7a80ab3d4f23676806b4f3a4f648088a63faadef06729daf5fcf808523df8ee.jpg)  
Figure is configured for 50-foot (15.2 m) TLOF  
Note 1: Arrowheads have constant dimensions.  
Note 2: If necessary, adjust stroke length to match length available. Minimum length = 10 ft (3 m).  
Note 3: Light type: omnidirectional green lights, Type L-861H or L-852H.

Note 4: If necessary, locate the lights outside of the arrow.

Note 5: In-pavement flight path alignment lighting is recommended.

Note 6: See paragraph 3.4 for guidance on flight path alignment markings.

## 3.5. Lighting.

Lighting is required for vertiports that support night operations. The lighting should enable the pilot to both establish the location of the vertiport and identify the perimeter of the operational area. In-pavement lighting is preferred to elevated lighting. The following guidelines apply to lighting:

## 3.5.1. General.

1. The FAA type L-861H omnidirectional perimeter light fixture supports all possible directions of approach. AC 150/5390-2 provides the standards for the FAA type L-861H light fixture.

2. For reference, the light fixtures are listed in AC 150/5390-2 as FAA type L-861H, elevated heliport perimeter light, and Type L-852H, in-pavement heliport perimeter light.

3. With light fixture FAA type L-861H as the base, elevated (FAA type L-861H) and in-pavement (FAA type L-852H) fixtures will be established in the next update of AC 150/5345-46, Specification for Runway and Taxiway Light Fixtures. Use FAA type L-861H for TLOF and FATO perimeter applications and for Flight Path Alignment Lights and Landing Direction Lights. See AC 150/5390-2 and AC 150/5345-46 for additional information.

4. The elevated light emitting diode (LED) vertiport fixture and LED in-pavement fixtures are identified as L-861H (L) and L-852H (L), respectively.

5. Perimeter light fixtures must meet chromaticity requirements for “aviation green” per SAE AS 25050, Colors, Aeronautical Lights and Lighting Equipment, General Requirements, when using incandescent lights. For light fixtures that use LEDs, see the standards in EB 67, Light Sources Other Than Incandescent and Xenon For Airport and Obstruction Lighting Fixtures.

6. Photometric standards for perimeter light fixtures are included in Table 3-1. See AC 150/5345-46, paragraph 3.3, Photometric Requirements, for detailed measurement methods and standards.

Table 3-1: Perimeter Lighting Intensity and Distribution
<table><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=2>Approach Angle0 to 15 degrees</td><td rowspan=1 colspan=1>Approach Angle16 to 90 degrees</td></tr><tr><td rowspan=1 colspan=1>Color</td><td rowspan=1 colspan=1>Minimum</td><td rowspan=1 colspan=1> Minimum average intensity</td><td rowspan=1 colspan=1>Minimum</td></tr><tr><td rowspan=1 colspan=1>Green</td><td rowspan=1 colspan=1>10 cd</td><td rowspan=1 colspan=1>15 cd</td><td rowspan=1 colspan=1>5cd</td></tr></table>

![7bf8ba635bb514693d03f64b8ef70537d339eac6670a6be79a427b6a41f3c8c1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7bf8ba635bb514693d03f64b8ef70537d339eac6670a6be79a427b6a41f3c8c1.jpg)

7. Elevated perimeter light fixtures will be installed in a load-bearing light base (L-868, Size B) or non-load-bearing light base (L-867, Size B) per AC 150/5345-42, Specification for Airport Light Bases, Transformer Housings, Junction Boxes, and Accessories. Shallow base type light bases will not be used.

8. Installation of vertiport lighting is to be in accordance with AC 150/5340-30, Design and Installation Details for Airport Visual Aids.

## 3.5.2. In-Pavement Perimeter Lights on TLOF and FATO.

1. TLOF perimeter lights are green and FAA type L-861H (AC 150/5345-46) or FAA type L-852H. LED versions of FAA type L-861H and L-852H are per AC 150/5345-46 and EB 87.

2. A square TLOF has:

a. One light in each corner.

b. Lights uniformly spaced between the corners with no less than five lights on each side.

c. Lights spaced no more than 25 feet (7.6 m) apart.

d. A light along the centerline of the approach.

3. A circular TLOF has:

a. An even number of lights

b. Minimum of eight lights uniformly spaced.

4. TLOF lights are within 1 foot (0.3 m) inside or outside of the perimeter line.

5. TLOF lights are installed in accordance with AC 150/5340-30.

6. Flight path alignment arrow lighting is recommended for night operations and includes a minimum of three lights spaced 5-10 feet (1.5 to 3 m) apart. These lights may extend across the TLOF, FATO, Safety Area, or any suitable surface in the immediate vicinity of the FATO or Safety Area, if necessary.

7. FATO perimeter lights are optional.

8. If installed, FATO perimeter lights are green and FAA type L-861H (AC 150/5345- 46) or FAA type L-852H. LED versions of FAA type L-861H and L-852H are per AC 150/5345-46 and EB 87.

9. A square FATO has:

a. One light in each corner.

b. Lights uniformly spaced between the corners with no less than five lights on each side.

c. Lights spaced no more than 25 feet (7.6 m) apart.

d. A light along the centerline of the approach.

10. A circular FATO has:

a. An even number of lights

b. Minimum of 8 lights uniformly spaced.

11. FATO lights are within 1 foot (0.3 m) of the inside or outside of the perimeter line.

12. Approach lights are optional. When installed they include a line of five green, omnidirectional lights located on the centerline of the preferred approach/departure path. The first light is 30 to 60 feet (9.1 to 18.3 m) from the TLOF. Remaining lights are spaced at 15-foot (4.6 m) intervals aligned on the centerline of the approach path.

See Figure 3-7 for additional guidance on perimeter lighting for surface level vertiports.   
See Figure 3-8 and Figure 3-9 for guidance for lighting for elevated vertiports.

Figure 3-7: TLOF/FATO Perimeter Lighting  
![43ecbc7907d9d32828a298c3dc0db38efdf6d710bd4ae5b9f322cf0e45ac37ec.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/43ecbc7907d9d32828a298c3dc0db38efdf6d710bd4ae5b9f322cf0e45ac37ec.jpg)  
Note 1: In-pavement lights are within 1 foot (0.3 m) of the inside or outside of the TLOF and FATO respective perimeters.

Note 2: Elevated lights are outside and within 10 feet (3 m) of TLOF and FATO respective perimeters.

Figure 3-8: Elevated Vertiport Configuration Example  
![935e701d50388b0e590bebb7758c121481addd4a74f4abe4845153375084a3c8.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/935e701d50388b0e590bebb7758c121481addd4a74f4abe4845153375084a3c8.jpg)  
Note: See Figure 3-9 for safety net and lighting details.

Figure 3-9: Elevated FATO Perimeter Lighting  
![7877e01b32f91e425ce353f13c639d43fa57d4794de28066841702f8a37adcef.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7877e01b32f91e425ce353f13c639d43fa57d4794de28066841702f8a37adcef.jpg)

Note 1: Install either “A” Type L-852H, or “B” Type L-861H.

Note 2: In-pavement edge light fixture Ⓐ (Type L-852H).

Note 3: Omnidirectional light Ⓑ, mounted off the structure edge (Type L-861H).

Note 4: Ensure elevated lights do not penetrate a horizontal plane at the TLOF elevation by more than 2 inches (51 mm).

Note 5: For TLOF and FATO lighting standards, see EB 87.

Note 6: A safety net’s supporting structure should be located below the safety net.

## 3.5.3. Elevated Perimeter Lights on TLOF and FATO.

The same standards for in-pavement lights apply to raised lights except for the following:

1. Lights are omnidirectional.

2. Lights are on the outside edge of the TLOF and FATO.

3. Lights are on frangible elevated light fixtures, no more than 8 inches (203 mm) high, and no more than 10 feet (3 m) out from the TLOF and FATO, respective, perimeters.

4. Lights do not penetrate a horizontal plane at the TLOF edge elevation by more than 2 inches (51 mm), as shown in Figure 2-2.

See Figure 3-7 for additional information.

## 3.5.4. Visual Glideslope Indicators (VGSI).

A VGSI provides pilots with visual vertical course and descent cues. Install the VGSI such that the lowest on-course visual signal provides a minimum of one degree of clearance over any object that lies within ten degrees of the approach course centerline.

## 3.5.4.1. Siting.

1. The optimum location of a VGSI is on the extended centerline of the approach path at a distance that brings the VTOL to a hover with the undercarriage between 3 and 8 feet (0.9 to 2.4 m) above the TLOF.

2. To properly locate the VGSI, estimate the vertical distance from the undercarriage to the pilot’s eye.

## 3.5.4.2. Control of the VGSI.

Design the VGSI to be pilot controllable such that it is “on” only when needed as an option.

## 3.5.4.3. VGSI Needed.

A VGSI is an optional feature. However, install a VGSI if one or more of the following conditions exist, especially at night:

1. Obstacle clearance, noise abatement, or traffic control procedures necessitate a slope to be flown.

2. The environment of the VTOL provides few visual surface cues.

## 3.5.4.4. Additional Guidance.

Additional guidance is provided in AC 150/5345-52, Generic Visual Glideslope Indicators (GVGI), and AC 150/5345-28, Precision Approach Path Indicator (PAPI) Systems.

## 3.5.5. Floodlight Option.

The FAA has not evaluated floodlights for effectiveness in visual acquisition of a vertiport. Guidelines for the use and installation of floodlights include:

1. Install floodlights to illuminate the TLOF, the FATO, and/or the parking area if ambient light does not suitably illuminate markings for night operations.

2. Mount these floodlights on adjacent buildings to eliminate the need for tall poles, if possible. Place floodlights clear of the TLOF, the FATO, the Safety Area, the approach/departure surfaces, and transitional surfaces and ensure floodlights and their associated hardware do not constitute an obstruction hazard.

3. Aim floodlights down to provide adequate illumination on the apron and parking surface.

4. Ensure floodlights that might interfere with pilot vision during takeoff and landings are capable of being turned off by pilot control or at pilot request.

Note 1: Floodlights do not replace TLOF or FATO lighting recommendations.

Note 2: White lighting for heliport applications should not be activated until the aircraft has landed and deactivated prior to takeoff.

## 3.6. Identification Beacon.

An identification beacon is required for night operations. The identification beacon is flashing white/yellow/green with a rate of 30 to 45 flashes per minute. On-airport vertiports are not required to have a vertiport identification beacon. Install beacons per the heliport guidance below:

1. AC 150/5345-12, Specification for Airport and Heliport Beacons, provides specifications for a beacon.

2. AC 150/5340-30 provides guidelines for installing a beacon.

## 3.7. Wind Cone.

Wind cones provide the direction and magnitude of the wind. The following guidelines apply to wind cones:

1. Minimum of one wind cone conforming to AC 150/5345-27, Specification for Wind Cone Assemblies.

2. Orange in color to provide the best possible contrast to its location’s background.

3. Locate to provide valid wind direction and speed information near the vertiport under all wind conditions.

4. Visible to pilots on the approach path when the aircraft is 500 feet (152 m) from the TLOF.

5. Visible to pilots from the TLOF.

6. Located within 500 feet (152 m) horizontal of the TLOF.

7. If one location does not provide for all the above, multiple locations may be necessary to provide pilots with all the wind information needed for safe operations.

8. See AC 150/5345-27 and AC 150/5340-30 for primary and secondary wind cones for multiple wind cone requirements.

9. Located outside the Safety Area and does not penetrate the approach/departure or transitional surfaces.

10. Follows installation details specified in AC 150/5340-30.

11. Lighted internally or externally for night operations.

## 4.0 Charging and Electric Infrastructure.

Most early concepts of operation for AAM activity indicate the use of electric propulsion by VTOL aircraft. The electrical needs for these aircraft vary based on design and manufacturer. This EB addresses battery driven technologies. Future guidance will be provided on other emerging energy concepts (e.g., hydrogen).

Electrification of aviation propulsion systems is an evolving area with few industryspecific standards. In addition to relevant national, state, and local building codes, the following sections provide a partial list of relevant standards that may assist when specifying charging systems and facility layout for this emerging industry. Current charging standards for light duty vehicle charging (up to 350kw) align with multiple light electric aircraft currently applying for certification. However, for meeting operational characteristics of higher capacity batteries and novel systems, manufacturers and operators may implement, along with fixed-charger equipment, alternate charging methods including mobile charging systems, fixed battery storage, cable and/or on-board battery cooling, battery swapping, or other concepts.

At the time of this publication, consensus has not been achieved regarding classes of charging or connection standards and could vary based on the aircraft duty cycle, charging speed, battery chemistry, charging system, and battery cooling system, etc. Charging infrastructure design for vertiports should consider adapting to multiple aircraft specific systems. Additional guidance is currently being developed as the AAM industry continues to evolve.

Battery charging must be done in a safe and secure manner. Any aircraft batteries stored on site should be stored safely away from TLOF, FATO, and Safety Areas. As additional research is developed, further recommendations will be released.

## 4.1. Standards.

4.1.1. Airport/Vertiport Fire Fighting and Safety Considerations.

2021 International Fire Code (IFC): To implement alternative energy vectors, there is the need for general precautions, emergency planning and preparedness, and storage of hazardous materials.

NFPA 110, Standard for Emergency and Standby Power Systems: To ensure the continuity of electric aircraft operations, uninterrupted power supply is needed thus creating a need for guidelines on emergency and backup power supply systems.

NFPA 70, NEC Article 625 - Electric Vehicle Charging System: Covers the electrical conductors and equipment external to an electric vehicle that connect an electric vehicle to a supply of electricity by conductive or inductive means, and the installation of equipment and devices related to electric vehicle charging. It also addresses scenarios that would allow the use of load balancing functions on electrical supply systems.

NFPA 70, Article 706 - Energy Storage Systems: This article applies to all energy storage systems (ESS) having a capacity greater than 3.6 MJ (1 kWh) that may be standalone or interactive with other electric power production sources. These systems are primarily intended to store and provide energy during normal operating conditions.

NFPA 400, Hazardous Materials Code: Covers the minimum NFPA standards for the storage and handling of hazardous materials such as lithium batteries.

NFPA 418, Standard for Heliports: This standard establishes fire safety standards for operations of heliports and rooftop hangars for the protection of people, aircraft, and other property. Future editions of this standard will include electric mobility asset considerations.

NFPA 855, Standard for the Installation of Stationary Energy Storage Systems: Covers the minimum NFPA standards established for design, installation, and maintenance of a stationary energy storage system including battery storage systems.

## 4.1.2. Occupational Safety and Health Administration Considerations.

29 CFR Section 1910.176, Handling Materials – General: This standard provides the minimum requirements for the storage and handling of hazardous materials such as lithium batteries.

## 4.1.3. Power Quality Considerations.

IEEE 519-2014, IEEE Recommended Practice and Requirements for Harmonic Control in Electric Power Systems: The grid impact of high wattage charging stations needs to be considered when designing and adopting charging stations. This standard provides guidance in the design and compliance of power systems with nonlinear loads.

IEEE 1826-2020, IEEE Standard for Power Electronics Open System Interfaces in Zonal Electrical Distribution Systems Rated Above 100 kW: Airports require power, monitoring, information exchange, control, and protection of interfaces that are based on technological maturity, accepted practices, and allowances for future technology insertions such as the integration of electric aircraft.

## 4.1.4. Underwriter’s Laboratories (UL) Certifications Considerations.

The following standards focuses on certifying the components and safety of the systems.

UL 2202, Standard for Safety of Electric Vehicle (EV) Charging System Equipment: Covers conducting charging system equipment (600 volts or less) for recharging batteries in surface electric vehicles.

UL 2251, Standard Testing for Charging Inlets and Plugs: Covers plugs, receptacles, vehicle inlets, and connectors rated up to 800 amperes and up to 600 volts AC or DC, and intended for conductive connection systems, for use with electric vehicles.

UL 2580, Batteries for Use in Electric Vehicles: Covers electric equipment storage assemblies in electric powered vehicles.

UL 9540, Energy Storage System (ESS) Requirements - Evolving to Meet Industry and Regulatory Needs: This key standard encompasses the design, commissioning, operation, decommissioning, and emergency operations for all energy storage systems.

UL 9540a, Test Method.

## 4.1.5. Vehicle to Infrastructure Considerations.

SAE J1772, SAE Electric Vehicle and Plugin Hybrid Electric Vehicle Conductive Charge Coupler: This standard was developed to define the fit and function of a conductive coupler for use in charging electric vehicles. It was later expanded to include direct current (DC) charging through combined alternating current/direct current (AC/DC) physical connector referred to as the Combined Charging Standard (CCS).

SAE AIR7357, MegaWatt and Extreme Fast Charging for Aircraft (under development): This standard is a work in progress under SAE leadership and intended to provide a charging interface for battery packs from 150kWh-1MWh within aircraft.

Megawatt Charging System (MCS): The MCS is intended to extend the capabilities of the CCS to accommodate the charge rate demands of larger vehicles and thus serve the trucking and aviation sectors. Ratings should exceed 1MW (Max 1,250 volt and 3,000 ampere (DC)) while also addressing communication and controls using ISO/IEC 15118 and meeting UL 2251 touch safe standards.

ISO/IEC 15118-1:2019, Road Vehicles: Vehicle to Grid Communication Interface: This standard defines the digital communications protocol to be used for the charging of high voltage electric vehicle batteries from a charging station. Beyond the basic handshakes and charge control between a vehicle and a charging station, this standard also includes convenience and security layers that support the “plug and charge” experience. Additionally, it offers the potential to schedule and coordinate the charging demands with the grid conditions.

## 5.0 On-Airport Vertiports.

To support AAM operations, certain OEMs and operators are interested in developing vertiports on airports and modifying existing on-airport helicopter landing facilities. All federally obligated airport sponsors are required to ensure the safety, efficiency, and utility of the airport and to provide reasonable and not unjustly discriminatory access to all aeronautical users.

This chapter addresses design considerations for separate vertiport facilities on airports. VTOLs can operate on airports without interfering with airplane traffic and operations. Operations can occur on existing airport infrastructure for its intended purpose or on dedicated vertiport facilities.

Separate vertiport facilities and approach/departure procedures may be needed when the volume of airplane and/or VTOL traffic affects operations. Airports with interconnecting passenger traffic between VTOLs and fixed wing aircraft should generally provide access between the respective terminals for boarding with applicable security measures in place.

Any new vertiport infrastructure or fixed equipment must be depicted on the ALP and submitted for FAA review prior to development and operation. For projects subject to FAA approval, an appropriate level of environmental review under the National Environmental Policy Act (NEPA) is required. These on-airport vertiport facilities must follow all guidance detailed in this EB.

For facilities being built on non-federally obligated airports, in compliance with Part 157, the sponsor or proponent must submit Form 7480-1 at least 90 days in advance of the day that construction work is to begin on the vertiport takeoff and landing area.

## 5.1. On-Airport Location of TLOF.

Locate the TLOF to provide ready access to the airport terminal with applicable security measures in place or to the VTOL user’s origin or destination. If needed, locate the TLOF away from but with access to fixed-wing aircraft movement areas (the runways, taxiways, and other areas of an airport that are used for taxiing, takeoff, and landing of aircraft, exclusive of loading ramps and aircraft parking areas).

## 5.2. On-Airport Location of FATO.

See Table 5-1 for standards of the distance between the centerline of an approach to a runway and the centerline of an approach to a vertiport’s FATO for simultaneous, samedirection VFR operations. Figure 5-1 depicts an example of an on-airport Vertiport location. The FATO should be located outside of all object free areas (OFAs), Safety Areas, runway protection zones, and safety critical navigational aid areas.

Table 5-1: Recommended Minimum Distance between Vertiport FATO Center to Runway Centerline for VFR Operations
<table><tr><td rowspan=1 colspan=1>ReferenceVTOL AircraftMTOW</td><td rowspan=1 colspan=1>Airplane Size</td><td rowspan=1 colspan=1>Distance FromVertiport FATO Centerto Runway Centerline</td></tr><tr><td rowspan=1 colspan=1>12,500 pounds(5,670 kg) or less</td><td rowspan=1 colspan=1>Small Airplane (12,500 pounds (5,670 kg) or less)</td><td rowspan=1 colspan=1>300 feet (91 m)</td></tr><tr><td rowspan=1 colspan=1>12,500 pounds(5,670 kg) or less</td><td rowspan=1 colspan=1>Large Airplane (12,500-300,000 pounds (5,670-136,079 kg))</td><td rowspan=1 colspan=1>500 feet (152 m)</td></tr><tr><td rowspan=1 colspan=1>12,500 pounds(5,670 kg) or less</td><td rowspan=1 colspan=1>Heavy Airplane (Over 300,000 pounds (136,079kg))</td><td rowspan=1 colspan=1>700 feet (213 m)</td></tr></table>

Figure 5-1: Example of an On-airport Vertiport  
![187982eedc80f7cf47c998f6ddafc8bda07a53ba2f11d315739988667c1756d0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/187982eedc80f7cf47c998f6ddafc8bda07a53ba2f11d315739988667c1756d0.jpg)  
Note: See Table 5-1.  
Note: Figure does not reflect every type of configuration.

## 6.0 Site Safety Elements.

## 6.1. Fire Fighting Considerations.

The procedures to put out a battery system fire on an aircraft may differ from one VTOL to another. Previous FAA research with small lithium battery cells found that water and other foam fire extinguishing agents were more effective for suppressing lithium battery fires and preventing thermal runaway than gas or dry powder extinguishing agents during experiments within a 4-foot (1.2 m) by 4-foot (1.2 m) by 4-foot (1.2 m) test chamber§§. The cooling effect of the extinguishing agent was the key factor in preventing the fire from spreading. Although this method was found to be effective for small battery packs, it is yet to be determined if similar results would be achieved with large battery packs.

The firefighting techniques for VTOL aircraft are still unknown and may differ from model to model. Providing adequate fire protection for VTOL aircraft on vertiports will require a full understanding of the hazards related to the specific aircraft that will be using the vertiport. This also applies to the utility infrastructure needed to charge the VTOL aircraft.

Vertiport operators may need to comply with applicable local fire, environmental, and zoning regulations. Vertiport operators will need the means to control VTOL aircraft fires. Firefighting personnel, including local first responders, should be trained and equipped to manage the specific needs associated with electric aircraft such as lithium battery fires, electrical fires, toxic gas emissions, and high voltage electrical arcing.

Firefighting equipment should be adjacent to, but outside, the TLOF and FATO area. Fire safety equipment should be clearly marked for conspicuousness from anywhere within or outside the FATO. For elevated sites, fire equipment may be located below the level of the FATO but must be fully accessible under all circumstances and clearly marked to anyone on the TLOF and FATO.

The current NFPA 418, Standard for Heliports (2021), is based on conventional liquid fuel and its dangers and risks. This standard is currently under revision to account for electrical hazards and fire safety standards for vertiports, which is expected to be published on or before January 2024. NFPA 855-2020, Standard for Stationary Energy Storage Systems, provides safety standards for stationary and mobile energy storage systems. Chapters on emergency response provide relevant guidance for fire protection engineers, system designers, code officials, and emergency responders.

## 6.2. Security and Safety.

For vertiports located in secured airport environments, unless screening was carried out at the VTOLs passengers’ departure location, Transportation Security Administration regulations may require that a screening area and/or screening be provided before passengers enter the airport’s secured areas. If necessary, airports should establish multiple VTOL parking positions and/or locations in the terminal area to service VTOL passenger screening and/or cargo needs. General information about passenger screening is available on the Transportation Security Administration website, www.tsa.gov/public/.

Controlling vertiport access and keeping operational areas clear of people, animals, equipment, debris, and vehicles is important for safety and security. The following guidance apply to safety barriers and access control measures:

1. For ground-level vertiports, erect a safety barrier around the VTOL aircraft operational areas in the form of a fence or a wall outside of the Safety Area and below the 8:1 elevation of the approach/departure surface.

2. If necessary, near the approach/departure paths, install the barrier well outside the outer perimeter of the Safety Area and below the elevation of the approach/departure and transitional surfaces described in paragraph 2.5.

3. Safety barriers must be high enough to present a positive deterrent to persons inadvertently or maliciously entering an operational area, but at a low enough elevation to be non-hazardous to all aircraft operations.

4. Provide control access to airport airside areas with adequate security measures as required or recommended by the Transportation Security Administration.

5. Display a vertiport caution sign like that shown in Figure 6-1 at all vertiport access points.

For on-airport vertiports, proponents should work with their local Transportation Security Administration security representative.

![1019ce4e3ae1c7c700b7949933c000a120879ff93fbbb3922f3a847dba7046e4.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/1019ce4e3ae1c7c700b7949933c000a120879ff93fbbb3922f3a847dba7046e4.jpg)

## 6.3. Downwash/Outwash.

The downwash and outwash impacts of VTOL are still being researched. However, the impacts of the ground geometry, surrounding infrastructure, and the re-circulatory flow impact on rotor/propeller aerodynamics performance and vehicle flight dynamics should still be considered in vertiport siting.

If downwash and outwash of the VTOL will create safety issues for people or property, other aircraft operators, or if the VTOL aircraft aerodynamic performance will be impacted by how the downwash and outwash interacts with the surrounding ground or infrastructure, then the TLOF, FATO, and Safety Areas should be adjusted appropriately, or alternative mitigations should be taken.

## 6.4. Turbulence.

Air (e.g., wind) flowing around and over buildings, stands of trees, terrain irregularities, and elsewhere can create turbulence on ground-level and rooftop vertiports that may affect VTOL operations. The following guidelines apply to turbulence:

1. When possible, locate the TLOF away from buildings, trees, and terrain to minimize air turbulence near the FATO and the approach/departure paths.

2. Assess the turbulence and airflow characteristics near and across the surface of the FATO to determine if a turbulence mitigating design measures are necessary (e.g., air gap between the roof, roof parapet, or supporting structure).

3. A minimum six-foot (1.8 m) unobstructed air gap on all sides above the level of the top of a structure (e.g., roof) and the elevated vertiport will reduce the turbdulent effect of air flowing over it.

4. Where an air gap or other turbulence-mitigating design measures are not taken on elevated structures, operational limitations may be necessary under certain wind conditions.

## 6.5. Weather Information.

An optional automated weather observing system (AWOS) measures and automatically broadcasts current weather conditions at the vertiport site. When installing an AWOS, locate it at least 100 feet (30.5 m) and not more than 700 feet (213 m) from the TLOF and such that its instruments will not be affected by rotor/propeller wash from VTOL operations. Find guidance on AWOS systems in AC 150/5220-16, Automated Weather Observing Systems (AWOS) for Non-Federal Applications, and FAA Order 6560.20, Siting Criteria for Automated Weather Observing Systems (AWOS). Other weather observing systems will have different siting criteria.

## 6.6. Winter Operations.

Swirling snow dispersed by an VTOL’s rotor/propeller wash can cause the pilot to lose sight of the intended landing point and/or obscure objects that need to be avoided. Elevated heliports may use a resistive heating system.

1. Design the vertiport to accommodate the methods and equipment to be used for snow removal.

2. Design the vertiport to allow the snow to be removed sufficiently so it will not present an obstruction hazard.

3. For vertiports in winter weather, an optional dark TLOF surface can be used to absorb more heat from the sun and melt residual ice and snow.

4. Find guidance on winter operations in AC 150/5200-30, Airport Field Condition Assessments and Winter Operations Safety.

## 6.7. Access to Vertiports by Individuals with Disabilities.

Congress has passed various laws concerning access to airports. Since vertiports are a type of airport, these laws are similarly applicable. Find guidance in AC 150/5360-14, Access to Airports by Individuals with Disabilities.

## Acronym List

<table><tr><td>AAM</td><td>advanced air mobility</td></tr><tr><td>AC</td><td>Advisory Circular</td></tr><tr><td>AC</td><td>alternating current</td></tr><tr><td>AGL</td><td>above ground level</td></tr><tr><td>ALP</td><td>Airport Layout Plan</td></tr><tr><td>AWOS</td><td>automated weather observing system</td></tr><tr><td>CCS</td><td>combined charging standard</td></tr><tr><td>CFR</td><td>Code of Federal Regulations</td></tr><tr><td>D</td><td>controlling dimension</td></tr><tr><td>DC</td><td>direct current</td></tr><tr><td>EB</td><td>Engineering Brief</td></tr><tr><td>ESS</td><td>energy storage system</td></tr><tr><td>ETL</td><td>effective translational lift</td></tr><tr><td>EV</td><td>electric vehicle</td></tr><tr><td>eVTOL</td><td>electric vertical takeoff and landing</td></tr><tr><td>FAA</td><td>Federal Aviation Administration</td></tr><tr><td>FATO</td><td>final approach and takeoff area</td></tr><tr><td>FC</td><td>failure condition</td></tr><tr><td>GA</td><td>general aviation</td></tr><tr><td>HOGE</td><td>hover out of ground effect</td></tr><tr><td>IEC</td><td>International Electrotechnical Commission</td></tr><tr><td>IEEE</td><td> Institute of Electrical and Electronics Engineers</td></tr><tr><td>IFC</td><td>International Fire Code</td></tr><tr><td>IFR</td><td> instrument flight rules</td></tr><tr><td>ISO</td><td>International Organization for Standardization</td></tr><tr><td>LAP</td><td>Landing Area Proposal</td></tr><tr><td>LDR</td><td>landing distance required</td></tr><tr><td>LED</td><td>light emitting diode</td></tr><tr><td>LOB</td><td>line of business</td></tr><tr><td>MCS</td><td>megawatt charging system</td></tr><tr><td>MSL</td><td>mean sea level</td></tr><tr><td>MTOW</td><td>maximum takeoff weight</td></tr><tr><td>NEC</td><td>National Electric Code</td></tr><tr><td>NEPA</td><td>National Environmental Policy Act</td></tr><tr><td>NEMSPA</td><td>National EMS Pilots Association</td></tr><tr><td>NFPA</td><td>National Fire Protection Association</td></tr><tr><td>OEM</td><td>original equipment manufacturer</td></tr><tr><td>OFA</td><td>object free area</td></tr><tr><td>RTODR</td><td>rejected takeoff distance required</td></tr><tr><td>SAE</td><td>SAE International</td></tr><tr><td>TDP</td><td>takeoff decision point</td></tr><tr><td>TLOF</td><td>touchdown and liftoff area</td></tr><tr><td>TODR</td><td>takeoff distance required</td></tr><tr><td>TSA</td><td>Transportation Security Administration</td></tr><tr><td>UL</td><td>Underwriters Laboratories</td></tr><tr><td>VFR</td><td>visual flight rule</td></tr><tr><td>VGSI</td><td>Visual Glideslope Indicator</td></tr><tr><td>VMC</td><td>visual meteorological conditions</td></tr><tr><td>VTOL</td><td>vertical takeoff and landing</td></tr></table>

# CASA Vertiport设计指南

# CASA AC139.V-01 Guidance on Vertiport Design (2023)

## ADVISORY CIRCULAR AC 139.V-01v1.0

Guidance for vertiport design

Advisory circulars are intended to provide advice and guidance to illustrate a means, but not necessarily the only means, of complying with the Regulations, or to explain certain regulatory requirements by providing informative, interpretative and explanatory material.

Advisory circulars should always be read in conjunction with the relevant regulations.

## Audience

This advisory circular (AC) applies to:

persons involved in the design, construction, and operation of vertiports

proponents of vertiports

AAM aircraft owners/operators

planning authorities

aerodrome operators

the Civil Aviation Safety Authority (CASA).

## Purpose

This AC provides initial guidance in the planning and physical design of vertiports to support the safe and efficient operation of vertical take-off and landing (VTOL) capable aircraft operating with a pilot on board in visual conditions only.

This AC is not intended to restrict or limit a pilot from determining the most suitable area for landing or take-off for the VTOL-capable aircraft operation.

Where possible, outcome-based guidance is provided. While regulations were previously written in a prescriptive manner , organisations are now also required to develop processes that will deliver an effective outcome.

For more information on understanding outcome-based legislation see AC 1-01 - Understanding the legislative framework.

## For further information

For further information, contact CASA’s Personnel Licensing, Aerodromes and Air Navigation Standards (telephone 131 757).

Unless specified otherwise, all subregulations, regulations, Divisions, Subparts and Parts referenced in this AC are references to the Civil Aviation Safety Regulations 1998 (CASR).

## Status

This version of the AC is approved by the Branch Manager, Flight Standards.

<table><tr><td colspan="3">Version Date</td></tr><tr><td>v1.0</td><td>July 2023</td><td>Details Initial AC.</td></tr></table>

## Contents

1 Reference material 4   
1.1 Acronyms 4   
1.2 Definitions 4   
1.3 References 7   
2 Introduction 8   
2.1 Background 8   
2.2 Site selection 8   
3 Vertiport physical characteristics 11   
3.1 General 11   
3.2 Essential vertiport components 12   
3.3 Optional vertiport components 14   
4 Obstacle limitation surfaces (OLS) 19   
4.1 Introduction 19   
4.2 Obstacle limitation surfaces origins 19   
4.3 Surfaces 21   
5 Visual aids 25   
5.2 Markers and markings - General 25   
5.3 Markers and markings - FATOs 25   
5.4 Markers and markings - taxiways and stands 32   
5.5 Visual aids - Lighting 34   
5.6 Machine-readable visual aids 39

## 1 Reference material

## 1.1 Acronyms

The acronyms and abbreviations used in this AC are listed in the table below.

<table><tr><td>Acronym</td><td>Description</td></tr><tr><td>AAM</td><td>Advanced Air Mobility</td></tr><tr><td>AC</td><td>advisory circular</td></tr><tr><td>AFM</td><td>aircraft flight manual</td></tr><tr><td>AIP</td><td>aeronautical information publication</td></tr><tr><td>CASA</td><td>Civil Aviation Safety Authority</td></tr><tr><td>CASR</td><td>Civil Aviation Safety Regulations 1998</td></tr><tr><td>FATO</td><td> final approach and take-of area</td></tr><tr><td>FOD</td><td>foreign object debris</td></tr><tr><td>FPA</td><td>FATO protection area</td></tr><tr><td>FPAGLS</td><td>Flight path alignment guidance lighting system(s)</td></tr><tr><td>ICAO</td><td>International Civil Aviation Organization</td></tr><tr><td>MOS</td><td>Manual of Standards</td></tr><tr><td>MTOW</td><td>maximum take-off weight</td></tr><tr><td>NASF</td><td>national airports safeguarding framework</td></tr><tr><td>OFV</td><td>obstacle free volume</td></tr><tr><td>OLS</td><td>obstacle limitation surface</td></tr><tr><td>RTODRV</td><td>rejected take-off distance required (for VTOL-capable aircraft)</td></tr><tr><td>SARPS</td><td>standards and recommended practices</td></tr><tr><td>TDPC</td><td>touchdown/positioning circle</td></tr><tr><td>TDPM</td><td>touchdown/positioning marking</td></tr><tr><td>TLOF</td><td>touchdown and lift off area</td></tr><tr><td>UCW</td><td>undercarriage width</td></tr><tr><td>VCA</td><td>VTOL-capable aircraft</td></tr><tr><td>VPS</td><td>vertical procedure surface</td></tr><tr><td>VPT</td><td>vertiport</td></tr><tr><td>VTOL</td><td>vertical take-off and landing</td></tr></table>

## 1.2 Definitions

Terms that have specific meaning within this AC are defined in the table below. Where definitions from the civil aviation legislation have been reproduced for ease of reference, these are identified

by 'grey shading'. Should there be a discrepancy between a definition given in this AC and the civil aviation legislation, the definition in the legislation prevails.
<table><tr><td>Term</td><td>Definition</td></tr><tr><td>Aerodrome</td><td>An area on land or water (including any buildings, installations, and equipment), the use of which as an aerodrome is authorised under the regulations, being such an area intended to be used either wholly or in part for the arrival, departure, and movement of aircraft.</td></tr><tr><td>Barrette</td><td>means 3 or more lights closely spaced in a transverse line so that from a distance they appear as a short bar of light.</td></tr><tr><td>D</td><td>for VTOL-capable aircraft, means the diameter of the smallest circle enclosing the aircraft projected on a horizontal plane, while the aircraft is in the take-off or landing configuration, with lift/thrust units turning, if applicable.</td></tr><tr><td></td><td>Note: If the aircraft changes dimensions during taxing or parking (e.g. folding wings), a corresponding Dtaxing or Dparking should also be provided.</td></tr><tr><td>Design D Design aircraft</td><td>the D of the design aircraft. means a virtual aircraft type that has the largest set of dimensions, the</td></tr><tr><td></td><td>greatest maximum take-off weight (MTOW), and the most critical obstacle avoidance criteria of the aircraft that the vertiport, or for a defined area within the vertiport, is intended to serve.</td></tr><tr><td>Downwash protection zone</td><td>The downwash protection zone is designed to protect the general public, other aircraft and those working in the immediate vicinity of operating VCA from the effect of buffeting.</td></tr><tr><td>D-Value</td><td>A limiting dimension, in terms of D, for a vertiport, or for a defined area within the vertiport.</td></tr><tr><td>Elevated vertiport</td><td>is a vertiport with a FATO location that would introduce a risk of fall from height or introduces a hazard to aircraft operations or to other people within the structure under the vertiport.</td></tr><tr><td>Elongated</td><td>when used with TLOF or FATO, elongated means an area which has a length more than twice its width.</td></tr><tr><td>Essential objects permitted</td><td>includes, but may not be limited to, around the touchdown and lift-off area (TLOF), perimeter lights and floodlights, guttering and raised kerb, foam monitors or ring-main system, handrails and associated signage, other lights.</td></tr><tr><td>off area (FATO) a.</td><td>Final approach and take- For the operation of a VTOL-capable aircraft, is defined as a solid area: from which a take-off is commenced;</td></tr><tr><td>Lighting element</td><td>or b. over which the final phase of approach to hover is completed. A lighting element is a light source within a lighting segment that may be</td></tr><tr><td></td><td>discrete (e.g., a Light Emitting Diode (LED)) or continuous (e.g., fibre optic cable, electro luminescent panel). An individual lighting element may consist of a single light source or multiple light sources arranged in a group or cluster and may include a lens/diffuser.</td></tr><tr><td>Lighting segments</td><td>Lighting segments are low profile lighting fixtures that consists of a line of lighting elements within unit or frame. For the purposes of this circular, the dimensions of a lighting segment are the</td></tr><tr><td></td><td>(LPs) are examples of lighting segments.</td></tr><tr><td>Obstacle</td><td>An object (whether temporary or permanent) or part of such an object that:</td></tr><tr><td></td><td>a. is located on an area provided for the movement of aircraft; or</td></tr><tr><td></td><td>b. extends above a defined surface designated to protect aircraft in flight</td></tr><tr><td>Obstacle free volume (OFV)</td><td>is a defined volume of airspace between the FATO protection area and the VPS, designed to protect aircraft conducting vertical procedures.</td></tr><tr><td>Protection area</td><td>means a defined area on a vertiport, which surrounds either the FATO or a stand, intended to reduce the risk of damage to an aircraft diverging from the</td></tr><tr><td>Reference circle</td><td>FATO or stand. is a horizontal circle, of the specified dimension, that is centred on any intended position/flight path at or above the applicable area/surface.</td></tr><tr><td>Rejected take-off distance required (RTODRV)</td><td>means the horizontal distance that is required from the start of the take-off to the point where the aircraft comes to a full stop, following a critical failure that is recognised at the TDP.</td></tr><tr><td>Take-off decision point (TDP)</td><td>means the first point that is defined by a combination of speed and height from which a safe take-off can be continued following a critical failure and is the last point in the take-off path from which a rejected take-off is ensured.</td></tr><tr><td>Touchdown and lift-off area (TLOF)</td><td>an area where a VTOL-capable aircraft may touch down or lift off.</td></tr><tr><td>Touchdown/positioning circle (TDPC)</td><td>a TDPM in the form of a circle, which is used for omnidirectional positioning in a TLOF.</td></tr><tr><td>Touchdown/positioning marking (TDPM)</td><td>a marking or set of markings that provide visual cues for the positioning of an aircraft.</td></tr><tr><td>Vertical procedures</td><td>take-of and landing procedures that include an initial and/or final vertical profile. The profile may or may not include a horizontal component.</td></tr><tr><td>Vertical procedure surface (VPS)</td><td>a surface at which a VTOL-capable aircraft either: a. begins its arriving vertical procedure,</td></tr><tr><td></td><td>or b. ends its departing vertical procedure.</td></tr><tr><td>Vertiport elevation</td><td>the highest point of the FATO, or where there are multiple FATOs, the highest point of the highest FATO.</td></tr><tr><td>Vertiport</td><td>an area of land, water, or structure that is used or intended to be used for the landing, take-off, and movement of VTOL-capable aircraft, that meets or exceeds the specifications contained within this advisory circular.</td></tr><tr><td></td><td>For the purposes of this AC the term vertiport also includes vertihubs and</td></tr><tr><td>vertistops: a.</td><td>Vertihub: a vertiport with infrastructure for maintenance, repair, fuelling, and parking spaces for storage of VTOL-capable aircraft.</td></tr><tr><td></td><td>b. Vertistop: a vertiport intended for take-off and landing of VTOL- capable aircraft to drop off or pick up passenger or cargo, but where</td></tr><tr><td>Vertiport clearway</td><td>means a defined horizontal surface selected and/or prepared as a suitable area over which an aircraft, capable of continued safe flight after a critical failure, may operate between the FATO/VPS and the approach/climb-out surface inner edge.</td></tr><tr><td>VCA (VTOL-capable aircraft)</td><td>a heavier-than-air aircraft, other than aeroplane or helicopter, capable of performing vertical procedures by means of more than two lift/thrust units.</td></tr><tr><td>VCA stand</td><td>a defined area that is intended to accommodate aircraft for loading or unloading passengers, mail, or cargo, fuelling/charging, parking, or</td></tr><tr><td>VCA taxi-route</td><td>maintenance. a defined path that is established for the movement of aircraft from one part of a vertiport to another:</td></tr><tr><td></td><td>a. an air taxi-route: a marked taxi-route that is intended for air taxing; and</td></tr><tr><td></td><td>b. a ground taxi-route: a taxi-route that is intended for ground movement of aircraft centred on a VCA taxiway.</td></tr></table>

## 1.3 References

## Advisory material

CASA's advisory materials are available at https://www.casa.gov.au/publications-and-resources/guidance-materials

<table><tr><td>Document</td><td>Title</td></tr><tr><td>AC 1-01</td><td>Understanding the legislative framework</td></tr></table>

## 2 Introduction

## 2.1 Background

2.1.1 This advisory circular (AC) provides guidance on the design elements of vertiports. This document assumes initial operations of pilot-on-board vertical take-off and landing (VTOL) capable aircraft (VCA) flying visual operations only.

2.1.2 With Advanced Air Mobility (AAM) evolving rapidly, these specifications have been prepared to support the progress of necessary aerodrome infrastructure. The guidance outlined below is flexible and structured such that it can evolve with this emerging industry.

2.1.3 However, it should be noted that these specifications are subject to change as aircraft performance and other data becomes available. Likewise, international standards are also in development and may impact on this guidance. Any significant revision of this guidance will be subject to industry consultation.

2.1.4 In addition to this, the introduction of AAM may impact and be impacted by considerations outside of aviation safety. Vertiport owners and operators should refer to local, state and other federal agencies to ensure appropriate adherence to their requirements.

2.1.5 As the following specifications are focused on VCA, runway-type final approach and take-off areas (FATO) have not been considered in the development of this AC.

2.1.6 This AC is the first in a collection of guidance material to be published. Additional ACs and supplementary material will provide further detail on design concepts as well as address operational considerations such as inspections, emergency response, aeronautical data and obstacle control.

## 2.2 Site selection

## 2.2.1 Fundamental considerations

2.2.1.1 The selection of a vertiport site involves the consideration of a range of variables including intended aircraft types, area available, vertiport configuration and obstacle environment.

Note: Limitations and restrictions to certain activities, such as aviation, may be imposed by State, Territory or Local Government on properties or locations through planning schemes or environmental planning instruments.

Site locations for proposed vertiport locations should consider suitability from a land-use planning perspective including any limitations or restrictions that could apply to the site.

Information in this advisory circular is additional to any limitation or restriction to the use of a site imposed by State, Territory or Local Government.

2.2.1.2 Full consideration of some of these variables relies on effective engagement with a range of stakeholders. Vertiport operators should establish open communication channels with aircraft operators, government stakeholders, nearby aerodrome (including certified aerodromes, non-certified aerodromes, helicopter landing sites and vertiport) operators and, where appropriate, the local community.

2.2.1.3 The aircraft type or types that are expected to use the vertiport form the basis for most design considerations when developing a vertiport. Where the vertiport owner intends on supporting a single aircraft type, that aircraft type will be the design aircraft. For vertiports intended to service multiple aircraft, the design aircraft is a virtual aircraft composed of the most demanding characteristics of these aircraft include including the largest set of dimensions, the greatest maximum take-off weight (MTOW), and the most critical flight path requirements (i.e., approach/climb-out gradient and/or horizontal flight requirements following a critical failure).

Note: Additional considerations of design aircraft may include considerations other than those mentioned in 2.2.1.3. Other considerations may include undercarriage width, landing distance requirements, rejected take-off distance requirements and the impact of downwash and outwash when VCA are landing, manoeuvring on the vertiport or at take-off.

2.2.1.4 The vertiport area available and the intended scope of operations may impact on the vertiport configuration. The number of facilities, such as FATOs, taxi routes, stands and associated buildings, may be limited by the physical environment. This AC provides specifications for each vertiport facility associated with the operation of aircraft without establishing a standard vertiport layout.

2.2.1.5 The potential for vertiports to be constructed in a complex wind (turbulent) environment means that specific considerations should be made when a vertiport is to be established in the vicinity of buildings, and significant terrain.

2.2.1.6 For vertiports within obstacle-rich environments or that may be impacted by future development, careful consideration of preferred and/or future flight paths should be made in consultation with appropriate stakeholders.

2.2.1.7 A gap analysis has identified that potential vertiport locations may be subject to multiple federal, state and local government regulatory requirements, as well as requirements from non-government sources, and these requirements may vary between different vertiport locations and jurisdictions.

2.2.1.8 This AC does not, and cannot, cover all vertiport development considerations. Vertiport owners and operators should consult with appropriate stakeholders (such as federal, state and local government agencies) on topics that are outside of CASA's remit including but not limited to noise, security, environmental concerns, weather reporting and privacy.

2.2.1.9 A vertiport and VCA compatibility study should be undertaken as part of the introduction of a new VCA, or when the mode of VCA operation changes to ensure the facilities at the vertiport remain suitable for all VCA using the vertiport.

## 2.2.2 Proximity to other vertiports or other aerodrome infrastructure

2.2.2.1 Where vertiports are located within the vicinity of other vertiports or aerodromes, the siting and design of FATOs and their associated flight paths should carefully consider interactions between own vertiport traffic, and other vertiport and aerodrome traffic.

## 2.2.3 Downwash and outwash protection

2.2.3.1 The characteristics and impacts of VCA downwash and outwash type effects1 are still unknown, however vertiport designers and operators will need to take into consideration their potential effects during the design process.

2.2.3.2 A vertiport and its facilities should be designed and located to protect the following from damage or injurious effects of downwash/outwash type effects associated with VCA operating to/from the vertiport:

people

other aircraft

buildings

vehicles

equipment.

2.2.3.3 An evaluation of downwash/outwash type impacts should be carried out. The evaluation should consider the VCAs downwash/outwash characteristics, the specific local conditions and relevant wind comfort criteria for affected persons and facilities.

2.2.3.4 At vertiports intended to service multiple types of VCA, or VCA operated by different operators, a detailed safety assessment and an operational evaluation of individual aircraft types operating to/from a given vertiport may need to be considered.

2.2.3.5 Information on potential downwash and outwash characteristics may be sought from VCA manufacturers and VCA operators. The manner in which a VCA may be operated could vary the actual downwash/outwash experienced.

2.2.3.6 To avoid or reduce the potential of incidents and accidents associated with VCA downwash/outwash, downwash protection zones2 around vertiports in the form of boundaries, or areas of restriction/control on movement of persons during VCA operations, should be considered.

2.2.3.7 This downwash protection zone should recognise that, in addition to the hover over the landing point, downwash/outwash will be prevalent during the final approach to the hover, the initial take-off, and whenever the VCA is positioning to or away from the FATO.

Note: The combined risk from an aviation safety and occupational health and safety perspective may require supervision of vehicular and pedestrian traffic during VCA movements, provision of robust maintenance and foreign object damage (FOD) prevention processes, and safeguarding of the downwash/outwash protection zone from future development to reduce the likelihood of injury or third-party damage.

## 3 Vertiport physical characteristics

## 3.1 General

3.1.1 A vertiport consists of set of essential components or defined areas as well as some optional components. These are the basic building blocks of a vertiport, as shown in Figure 1, and include:

a. one or more FATO

b. one or more touch down and lift-off areas (TLOF)

c. protection areas

d. taxiways and/or taxi-routes

e. stands

3.1.2 The following specifications are based on the design assumption that no more than one VCA will be in the FATO at the same time.

3.1.3 Further, it is also assumed that operations to/from a FATO in proximity to another FATO will not be simultaneous. If simultaneous operations are planned, appropriate separation distances between FATOs should be determined with due regard to issues such as downwash, flight paths and other airspace limitations.

3.1.4 Safety devices to mitigate the risk of fall from height at elevated vertiports should not penetrate the OLS or exceed the height of the protection area.

![2bce03485079c508b352d34c25fe51bc40155e582d4a9d3384a6b55d0b04b8be.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/2bce03485079c508b352d34c25fe51bc40155e582d4a9d3384a6b55d0b04b8be.jpg)  
Figure 1 – Vertiport components

## 3.2 Essential vertiport components

## 3.2.1 Final approach and take-off (FATO) area

3.2.1.1 A vertiport should be provided with at least one FATO.

3.2.1.2 A FATO should have the following features:

a. A sufficient size and shape to ensure containment of every part of the design aircraft in the final phase of approach and commencement of take-off in accordance with the intended procedures. The shape of the FATO is optional as represented in Figures 1, 2 and 12.

b. When collocated with a touchdown and lift-off (TLOF) area, contiguous and flush with the TLOF, and meet the requirements of 3.2.2.3 b.

c. When non-collocated with a TLOF, free of obstacles, except for essential objects, free of hazards to a potential forced landing and resistant to the effects of downwash.

3.2.1.3 The dimensions of a FATO should be the:

a. length of the rejected take-off distance required (RTODRV) prescribed in the design aircraft flight manual (AFM), or 1.5 Design D, whichever is greater: and

b. width prescribed in the design aircraft AFM, or 1.5 Design D, whichever is greater.

3.2.1.4 Essential objects should not exceed 5 cm in height.

3.2.1.5 The slope of a FATO should not exceed 2 % in any direction.

3.2.1.6 A FATO should be located to minimize the influence of the surrounding environment, including turbulence, which could have an adverse impact on aircraft operations.

3.2.1.7 A FATO should be surrounded by a FATO Protection Area (FPA) as per 4.1.1.

3.2.1.8 Where a vertiport intends to have more than one FATO, the distance between any two proximate FATOs should be determined by a safety assessment that supports the safe operations of intended VCA movements.

Note: As VCA performance data becomes available, changes to FATO requirements such as minimum size or the requirement for the FATO being solid may be reviewed.

## 3.2.2 Touchdown and lift-off (TLOF) area

3.2.2.1 A vertiport should be provided with at least one TLOF.

3.2.2.2 A TLOF should be provided within a FATO as shown in Figure 2, or stand as shown in Figure 13c, whenever it is intended that the undercarriage of the VCA will touch down or lift off.

## 3.2.2.3 A TLOF should have the following features:

a. A sufficient size and shape to ensure containment of the undercarriage of the design aircraft aligned with the intended orientation.

b. An area which:

i. is free of obstacles

ii. has sufficient bearing strength to accommodate the dynamic loads associated with the design aircraft.

iii. is free of irregularities that would adversely affect the touchdown, lift-off or taxi of VCA

iv. has sufficient friction to avoid skidding of VCA or slipping of persons

v. is resistant to the effects of downwash

vi. ensures effective drainage while having no adverse effect on the control or stability of a VCA during touchdown, lift-off, or when stationary.

3.2.2.4 The minimum dimensions of a TLOF should be the dimensions prescribed in the design aircraft AFM, or 0.83 Design D, whichever is greater.

3.2.2.5 The slope of a TLOF should not exceed 2 % in any direction.

3.2.2.6 When a TLOF is within a FATO, it should be:

a. centred on the FATO, or

b. for an elongated FATO, centred on the longitudinal axis of the FATO.

3.2.2.7 When a TLOF is within a VCA stand, it should be centred on the stand.

![ea0ebedeb911b823dd959171531e6d0780aec45cd1dc17153ef84cefbf42d8f6.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ea0ebedeb911b823dd959171531e6d0780aec45cd1dc17153ef84cefbf42d8f6.jpg)  
Figure 2 - FATO, TLOF (with TDPC)

## 3.3 Optional vertiport components

## 3.3.1 VCA taxiways

3.3.1.1 A VCA taxiway should be provided for the intended ground movement of a VCA within the vertiport under its own power or by means of ground movement equipment.

3.3.1.2 A VCA taxiway should be located within a taxi-route and have the following features:

a. sufficient width to ensure containment of the undercarriage of the design aircraft; b. area which:

i. is free of obstacles

ii. has the bearing strength to accommodate the taxiing loads of the aircraft the taxiway is intended to serve

iii. is free of irregularities that would adversely affect the ground taxiing of a VCA

iv. is resistant to the effects of downwash

v. ensures effective drainage while having no adverse effect on the control or stability of a VCA when being manoeuvred under its own power, or by ground movement equipment, or when stationary.

3.3.1.3 The minimum width of a VCA taxiway should be two times the undercarriage width (UCW) of the design aircraft, as shown in Figure 3.

3.3.1.4 The transverse slope of a taxiway should not exceed 2 % and the longitudinal slope should not exceed 3 %.

3.3.1.5 When defining the distance between ground taxiways, the separation distance between an aircraft on a ground taxiway and an aircraft on a parallel ground taxiway or an object should take into consideration a minimum wingtip clearance of at least 0.25 maximum width of the design aircraft.

Note: Where taxiways are intended to be used by vehicles and equipment considerations should be made to taxiway width and bearing strength.

Wing tip to wing tip clearance (min 0.25 x max width)

![78f0cf6957aa48efb0c0fd376be6911bba6bcf52a4d21efd19965e1f54368e9c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/78f0cf6957aa48efb0c0fd376be6911bba6bcf52a4d21efd19965e1f54368e9c.jpg)  
Clearance to object (min 0.25 x max width)

![cc1db1800a2ac72181a5fc69f99c2f0c3274babc166228a7e7a120b6e4c5e411.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/cc1db1800a2ac72181a5fc69f99c2f0c3274babc166228a7e7a120b6e4c5e411.jpg)  
Ground taxi-route (1.5 x max width)

Figure 3 - VCA taxiways and clearance distances

## 3.3.2 Taxi routes for VCA

3.3.2.1 A VCA taxi-route should be provided for the intended movement of a VCA within the vertiport under its own power or by means of ground movement equipment.

## 3.3.2.2 A VCA taxi-route should have the following features:

a. sufficient width to ensure containment of the design aircraft

b. free of obstacles, except for essential objects

c. resistant to the effects of downwash

d. when collocated with a taxiway:

i. is contiguous and flush with the taxiway

ii. does not present a hazard to operations

iii. ensures effective drainage

iv. not exceed an upward transverse slope of 4 % outwards from the edge of the taxiway.

e. when not collocated with a taxiway, is free of hazards if a forced landing is required.

3.3.2.3 Where collocated with a taxiway, essential objects located in the VCA taxi-route should not:

a. be located at a distance of less than 50 cm outwards from the edge of the taxiway

b. penetrate a surface originating 50 cm outwards of the edge of the taxiway and a height of 25 cm above the taxiway and sloping upwards and outwards at a gradient of 5 % up to the outer edge of the ground taxi-route.

Note: Consideration of low-mounted lift/thrust units may be required to ensure that appropriate clearances are maintained.

## Ground taxi-routes for VCA

3.3.2.4 A VCA ground taxi-route should have a minimum width of 1.5 times the overall width of the design aircraft it is intended to serve and be centred on a taxiway, as shown in Figure 4.

Note: Where the VCA operating width differs (e.g. folding wings) while taxiing, the reduced width may be considered for defining the taxi-route width.

## Air taxi-route for VCA

3.3.2.5 A VCA air taxi-route should have a minimum width of twice the overall width of the design aircraft it is intended to serve, as shown in Figure 4.

3.3.2.6 When not collocated with a taxiway, the slopes of the ground below an air taxi-route should not exceed the slope landing limitations of the design aircraft the taxi-route is intended to serve. In any event, the transverse slope should not exceed 10 % and the longitudinal slope should not exceed 7 %.

Note: When determining the width of an air taxi route, the potential impact of downwash or outwash from an of air-taxiing VCA should be considered.

Ground taxi-route = 1.5 x overall width

![d4bb431e1a157903756f3ba4070cc979186b99c77dbada0e42f32919793aa617.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d4bb431e1a157903756f3ba4070cc979186b99c77dbada0e42f32919793aa617.jpg)  
Taxiway (min 2x UCW)

Air taxi-route = 2 x overall width  
![5ea43da5d4681b743c89b31325ad217237d6dc3b6a29f38ba3746e5578e27808.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5ea43da5d4681b743c89b31325ad217237d6dc3b6a29f38ba3746e5578e27808.jpg)  
Figure 4 - VCA taxi-routes

Air taxi-route = 2 x overall width  
![cbdd2c968cb297abe6d760259a7fbf8974e8c08aa47ec0b89f48c222d2d0966c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/cbdd2c968cb297abe6d760259a7fbf8974e8c08aa47ec0b89f48c222d2d0966c.jpg)

## 3.3.3 VCA stands

3.3.3.1 VCA stands may be provided to permit the safe loading and off-loading of passengers and/or cargo, as well as the servicing of the VCA without interfering with other traffic.

## 3.3.3.2 A VCA stand, as shown in Figure 6, should have the following features:

a. sufficient size and shape to ensure containment of every part of the design aircraft when it is being positioned within the stand

b. An area which:

i. Is free of obstacles

ii. has bearing strength capable of withstanding the intended loads

iii. is free of irregularities that would adversely affect the manoeuvring of VCA

iv. has sufficient friction to avoid skidding of VCA or slipping of persons

v. is resistant to the effects of downwash

vi. ensures effective drainage while having no adverse effect on the control or stability of a VCA when being manoeuvred under its own power, when being moved by means of ground movement equipment, or when stationary.

3.3.3.3 The slope of a VCA stand should not exceed 2 % in any direction.

## 3.3.4 D-Value-based VCA stand

3.3.4.1 When the VCA stand design is based on D-value, the minimum dimensions should be:

a. a circle of diameter of 1.2 Design D

or

b. when there is a limitation on manoeuvring and positioning, of sufficient width to meet the requirement of 3.3.3.2 (a) above, but not less than 1.2 times overall width of design aircraft.

3.3.4.2 A D-value based VCA stand should be located within a protection area.

## 3.3.5 Geometry-based VCA stand

3.3.5.1 For VCA that enter/exit the stand with surface movement either under own power or by means of ground movement equipment, where practical, stands may be designed in accordance with the geometry of the aircraft, as shown in Figure 5, following the aerodrome apron concept.

3.3.5.2 The clearances should be based on the dimensions of all the VCAs expected to use the stand.

3.3.5.3 The clearance distance between a VCA and other adjacent VCA, buildings or objects on the apron should be sufficient to meet the requirement of 3.3.3.2 (a) above, but not less than:

a. For VCA with a width of less than 18 m:

i. 3 m

or

ii. 0.25 the overall width of the widest VCA expected to use the stand, whichever is greater

b. For VCA with a width greater than 18 m not less than 4.5 m.

![62eb243650fb3b0bc47d4579c6f97f253820d3736763d56899770736a61c9d7c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/62eb243650fb3b0bc47d4579c6f97f253820d3736763d56899770736a61c9d7c.jpg)  
Figure 5 - Example of geometry-based stands (VCA less than 18m in width)

## 3.3.6 Protection areas for D-value-based VCA stands

3.3.6.1 A stand protection area should be provided for D-value-based VCA stands, as shown in Figure 6.

3.3.6.2 A protection area should have the following features:

a. free of obstacles, except for essential objects

b. resistant to the effects of downwash

c. when solid, flush with the stand, not exceed an upward slope of 4 % outwards from the edge of the stand and ensures effective drainage.

3.3.6.3 When associated with a stand designed for turning, the protection area should extend outwards from the periphery of the stand for a distance of 0.4 Design D. Otherwise, the minimum width of the stand and the protection area should not be less than the width of the associated taxi-route.

## 3.3.6.4 When associated with a stand designed for non-simultaneous aircraft operations:

a. the protection area of adjacent stands may overlap but should not be less than the required protection area for the larger of the adjacent standards

b. the adjacent stand may contain a static aircraft.

## 3.3.6.5 Essential objects located in the protection area should not:

a. If located at a distance of less than 0.75 Design D from the centre of the VCA stand, penetrate a surface at a height of 5 cm above the level of the stand.

b. If located at a distance of 0.75 Design D or more from the centre of the VCA stand, penetrate a surface at a height of 25 cm above the level of the stand and sloping upwards and outwards at a gradient of 5 %.

![390646cb91205a3328e6fd8f4c1deb8eaa7e16999db66dde57b3bb01dcada379.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/390646cb91205a3328e6fd8f4c1deb8eaa7e16999db66dde57b3bb01dcada379.jpg)  
Example A: Ground taxi. Simultaneous taxi-on/push-back stands

![68166d81937a59ccad0af5441ec14797db977ea5171275d0713227207f8ea03c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/68166d81937a59ccad0af5441ec14797db977ea5171275d0713227207f8ea03c.jpg)  
Example B: Ground taxi. Simultaneous turning stands

![0c89fa5f3ef6f5508683853e6822fd80a871a7d3f8986c20ae92e44ce580823f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0c89fa5f3ef6f5508683853e6822fd80a871a7d3f8986c20ae92e44ce580823f.jpg)  
Example C: Ground taxi. Non-simultaneous taxi-on/push-back stands dependent on other stand being clear or with static aircraft

![859cd526f516875e6e1e56d1eb9af8701eb1667fbc425ba433e87acd7d6062dd.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/859cd526f516875e6e1e56d1eb9af8701eb1667fbc425ba433e87acd7d6062dd.jpg)  
Example D: Ground taxi. Non-simultaneous turning stands dependent on other stand being clear or with static aircraft only

![1c91f26cb47246c1e98a00f4102966bf07f8d1784177389f30f781518622d315.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/1c91f26cb47246c1e98a00f4102966bf07f8d1784177389f30f781518622d315.jpg)  
Example E: Air taxi. Simultaneous taxi-through stands

![0b64b438760d1851c30c215c1ce1ba8cac1d9931a7c36486f02f3848be174193.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0b64b438760d1851c30c215c1ce1ba8cac1d9931a7c36486f02f3848be174193.jpg)  
Example F: Air taxi. Simultaneous turning stands

![a0ecc56905abe3e5b617cd56b82c8e6135b1a605400f4b7f8b7965567fc8472d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a0ecc56905abe3e5b617cd56b82c8e6135b1a605400f4b7f8b7965567fc8472d.jpg)  
Example G: Air taxi. Non-simultaneous taxi-through stands dependent on other stand being clear or with static aircraft only

![4c4437df1d49164c2aad80f302c7c727d0934ed108de6def1bf2ec38cf0cda1c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4c4437df1d49164c2aad80f302c7c727d0934ed108de6def1bf2ec38cf0cda1c.jpg)  
Example H: Air taxi. Non-simultaneous turning stands dependent on other stand being clear or with static aircraft only

Figure 6 - Protection areas for VCA stands and the associated VCA taxi-routes for different operational scenarios

## 4 Obstacle limitation surfaces (OLS)

## 4.1 Introduction

## 4.1.1 Establishing obstacle limitation surfaces

4.1.1.1 A vertiport operator should establish the obstacle limitation surfaces (OLS) applicable to the critical performance of the design VCA.

Note: Refer to AC 139.V-02 for the monitoring of obstacles in navigable airspace in the vicinity of the vertiport.

## 4.2 Obstacle limitation surfaces origins

4.2.1 The following section outlines the protected areas from which obstacle limitation surfaces (OLS) originate. The dimensions of the OLS serve a general objective of protection of approach, climb-out and balked landing manoeuvres in the visual phase of the approachto-land below a height of 152 m above the FATO elevation.

## 4.2.2 FATO Protection Area (FPA)

4.2.2.1 An FPA should be provided for each FATO, as shown in Figure 7.

4.2.2.2 An FPA should have the following features:

a. free of obstacles, except for essential objects

b. where solid, flush with the edge of the FATO, resistant to the effects of downwash and ensures effective drainage.

4.2.2.3 Where a FATO supports landing/take-off without vertical procedures, the FPA is an area surrounding the FATO that encompasses:

a. the area(s) bordered by a circumscribed square aligned with the landing/take-off flight path(s) centred on the FPA reference circle(s)

b. any area contained within the direct common tangents of any multiple FPA reference circles.

4.2.2.4 Where a FATO supports landing/take-off with vertical procedures only, the FPA is an area surrounding the FATO that encompasses:

a. the FPA reference circle(s)

b. any area contained within the direct common tangents of any multiple FPA reference circles.

4.2.2.5 The radius of an FPA reference circle should be half the FATO width plus 3 m or 0.25 Design D, whichever is greater.

4.2.2.6 Where the FATO length is greater than its width, separate FPA reference circles are centred on the FATO centreline at a distance of half the FATO width from the FATO ends, as shown in Example C of Figure 7.

4.2.2.7 Essential objects located in the FPA should not exceed 25 cm in height and should be frangibly mounted.

![cefc0895dae7c5966922f008bf338bbd4aab9ddf013d26932e99340b62f8a248.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/cefc0895dae7c5966922f008bf338bbd4aab9ddf013d26932e99340b62f8a248.jpg)  
Figure 7 - Protection surfaces for vertiports without vertical procedures

## 4.2.3 Vertical Procedure Surface

4.2.3.1 A vertical procedure surface (VPS) should be established for where vertical procedures are used for landing or take-off from the vertiport.

4.2.3.2 The VPS is a surface that encompasses the area bordered by a circumscribed square(s) aligned with the intended aircraft flight path(s) centred on the VPS reference circle, as shown in Figures 8, 9 and 11.

4.2.3.3 A VPS should be free of obstacles.

4.2.3.4 A VPS reference circle should be established above and centred on the FATO.

4.2.3.5 The diameter of a VPS reference circle should be the diameter of the associated FPA reference circle, plus 1 Design D per 100 ft increase in height above the FATO.

4.2.3.6 The vertiport operator should determine the elevation of the VPS subject to the performance characteristics of the most demanding VCA intended to use the vertiport or the VCA operator’s intended operational requirements.

## 4.2.4 Obstacle Free Volume (OFV)

4.2.4.1 An OFV should be established between a VPS and the associated FPA.

4.2.4.2 An OFV should be free of obstacles.

4.2.4.3 The OFV is a truncated cone extending between the edge of the FPA reference circle to the edge of the VPS reference circle, as shown in Figure 8, 9 and 11.

## 4.2.5 Vertiport clearway

4.2.5.1 A vertiport clearway should be established when a VCA needs to manoeuvre, horizontally, between the FPA/VPS outer edge and the approach/climb-out surface inner edge.

4.2.5.2 A vertiport clearway should have the following features:

a. sufficient size and shape to ensure containment of the design aircraft when it is operating between the FPA/VPS and the approach/climb-out surface

b. free of obstacles, except for essential objects

c. resistant to the effects of downwash

d. when at ground level, contiguous surface flush with the FPA, and free of hazards should a forced landing be required.

4.2.5.3 The width of a vertiport clearway should not be less than that of the associated FPA/VPS and centred on the intended flight path, as shown in Figure 7 and 11.

## 4.3 Surfaces

## 4.3.1 Approach/Climb-Out Surface

4.3.1.1 An approach/climb-out surface should be established for each approach and climb-out flight path to and from the vertiport, as shown in Figures 8 to 11.

4.3.1.2 The approach/climb-out surface consists of an inclined plane or a combination of planes or, when turns are involved, a complex surface, sloping upwards from the inner edge and centred on the intended flight path that must be clear of obstacles.

4.3.1.3 The limits of an approach/climb-out surface should comprise:

a. an inner edge coincident with and of equal length to the outer edge of the associated FPA/VPS/clearway

b. two side edges originating at the ends of the inner edge and diverging uniformly at a specified rate from the vertical plane, aligned with the intended flight path to a specified width and continuing thereafter at that width for the remaining length of the approach/climb-out surface

c. an outer edge horizontal and perpendicular to the centre line of the approach surface intended flight path at a specified height above the vertiport elevation.

4.3.1.4 The specified values of the above characteristics are outlined in table 2.

Table 2 - OLS surface values - Approach/climb-out surface characteristics
<table><tr><td rowspan=1 colspan=2>Characteristics                                                  Value</td></tr><tr><td rowspan=1 colspan=1>Inner edge width:</td><td rowspan=1 colspan=1>Width of FPA/VPS/clearway</td></tr><tr><td rowspan=1 colspan=1>Day use only final width:</td><td rowspan=1 colspan=1>7x Design D</td></tr><tr><td rowspan=1 colspan=1>Day use only divergence:</td><td rowspan=1 colspan=1>10%</td></tr><tr><td rowspan=1 colspan=1>Night use final width:</td><td rowspan=1 colspan=1>10x Design D</td></tr><tr><td rowspan=1 colspan=1>Night use divergence:</td><td rowspan=1 colspan=1>15%</td></tr><tr><td rowspan=1 colspan=1>Outer edge height above FATO elevation</td><td rowspan=1 colspan=1>500&#x27;(152m)</td></tr></table>

4.3.1.5 In the case of an approach/climb-out surface involving turns, the surface is a complex surface containing the horizontal normals to its centre line and the slope of the centre line should be the same as that for a straight approach surface.

4.3.1.6 The slope(s) of the approach/climb-out surface should be measured in the vertical plane containing the centre line of the surface.

4.3.1.7 The approach/climb-out surface slope or combination of slopes and section lengths should be determined with reference to the obstacle environment and intended aircraft performance capabilities. If multiple slope/sections are established, the divergent portion of the approach/climb-out surface should be a single consistent slope.

## 4.3.2 Transitional surface

4.3.2.1 A transitional surface should be established on each side of an approach/climb-out surface and its associated clearway/VPS/FPA, as shown in Figures 8 to 11.

4.3.2.2 The transitional surfaces should be clear of obstacles.

4.3.2.3 The transitional surface should comprise:

a. a lower edge beginning at the point on the outer edge of the approach/climb-out surface where it reaches its final width then extending downwards and along the side of the approach/climb-out surface to the inner edge and from there

b. where provided, along the side of the clearway parallel to intended flight path

c. along the length of the side of the VPS

d. along the length of the side of the FPA parallel to the intended flight path

e. an upper edge beginning at the point where the outer edge of the approach/climbout surface reaches its final width and then parallel to the intended flight path at a constant height.

Note: As the transitional surface is dependent on the approach/climb-out angle and Design D, it may extend the full length of the approach/climb-out surface. It may also be impacted by the extent of any vertical procedure such that it is no longer present.

![04ab6fd105c6d050f738b8cc4a3ba94318850dac581657b368a76542093861bb.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/04ab6fd105c6d050f738b8cc4a3ba94318850dac581657b368a76542093861bb.jpg)

![f054a0e8dd40667b0ab8e1d1764e1b69bd3ec027d46980411af2f594009a7fcf.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f054a0e8dd40667b0ab8e1d1764e1b69bd3ec027d46980411af2f594009a7fcf.jpg)  
Figure 8 - An example OLS design for a vertiport accommodating vertical procedures

![7f182fddb329f5a65bff42704df42588c1ebe6d49ddd93f1fc0662424bb17507.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7f182fddb329f5a65bff42704df42588c1ebe6d49ddd93f1fc0662424bb17507.jpg)  
Figure 9 - Illustration of a simple vertiport OLS. Showing an OFV, VPS, VPS reference circle, a single approach/climb-out surface and transitional surfaces

![bb2f8f8987ff67b6faeb8a1d4da7f3067831447eaf9c141e5bf9808a65ac6e8a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/bb2f8f8987ff67b6faeb8a1d4da7f3067831447eaf9c141e5bf9808a65ac6e8a.jpg)  
Figure 10 - Illustration of a simple elevated vertiport OLS. Showing an FPA, dual approach/climb-out surfaces and transitional surfaces

![3625b1e296265d1b8923f29b241879f01be6c7558a0ed9d2e246ff4be18384cc.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3625b1e296265d1b8923f29b241879f01be6c7558a0ed9d2e246ff4be18384cc.jpg)  
Figure 11 - Illustration of a complex vertiport OLS. Showing an FPA, OFV, FPA, clearway, dual approach/climb-out surfaces over the river and transitional surfaces

## 5 Visual aids

## 5.1.1 Wind direction indicators

5.1.1.1 A wind direction indicator should be provided at a vertiport to provide a visual indication of the wind direction and speed.

5.1.1.2 A wind direction indicator should be located to indicate the wind conditions over the FATO in such a way as to be free from the effects of airflow disturbances caused by nearby objects or downwash from the lift/thrust units. It should be visible from a VCA in flight, in hover or on the movement area.

5.1.1.3 A wind direction indicator sleeve should be a truncated cone made of lightweight fabric and should have the dimensions of 1.2 m in length, with a diameter of 0.3 m (at the larger end) to 0.15 m (at the smaller end).

5.1.1.4 The colour(s) of the wind direction indicator sleeve should such that it is clearly visible against its visual background.

5.1.1.5 A wind direction indicator at a vertiport intended for use at night should be lit such that it is clearly visible against its visual background.

## 5.2 Markers and markings - General

5.2.1.1 Markers and markings should be installed, in accordance with the following specifications, at a vertiport used or available for operations in daylight or at night.

5.2.1.2 Markers and markings should be clearly visible to the vertiport user by way of:

a. provision of a contrasting background marking (a box or border)

b. where allowed for in the specifications below, the selection of an appropriate contrasting colour

c. any other method that would increase the conspicuity of the marking or marker in operational conditions.

5.2.1.3 The night-time visibility of markers and markings may be supplemented by reflective/refractive material and/or electroluminescent paint providing that such material does not pose a hazard if dislodged.

## 5.3 Markers and markings - FATOs

## 5.3.1 Flight path alignment guidance marking

![eb3368b25005164f2c04bd2dc2cf9dbc0b166d19bc2a8f35caf7cf3b1af2c512.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/eb3368b25005164f2c04bd2dc2cf9dbc0b166d19bc2a8f35caf7cf3b1af2c512.jpg)  
Figure 12 - Flight path alignment guidance marking

5.3.1.1 Flight path alignment guidance marking(s) should be provided at a vertiport where it is desirable and practicable to indicate available approach and/or departure path direction(s).

5.3.1.2 The flight path alignment guidance marking should be located in a straight line along the direction of landing and/or take-off path to the FATO.

5.3.1.3 A flight path alignment guidance marking should consist of each of the following characteristics:

a. one or more arrows marked on the TLOF, FATO and/or FPA

b. the stroke of the arrow(s) shall be 0.5 m in width and at least 3 m in length

c. take the form shown in Figure 12 which includes the scheme for marking ‘heads of the arrows’ which are constant regardless of stroke length.

5.3.1.4 In the case of a flight path limited to a single landing direction or single take-off direction, the arrow marking may be unidirectional. In the case of a vertiport with only a single landing/take-off path available, one bidirectional arrow is marked. Both cases are shown in Figure 16b.

5.3.1.5 The marking should be white.

## 5.3.2 FATO Perimeter marking or markers

![5788cb85c975ece2ad358da9c696012c4663df0105e44b701e24fb69e3d8236e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5788cb85c975ece2ad358da9c696012c4663df0105e44b701e24fb69e3d8236e.jpg)  
Figure 13 – FATO perimeter markings/markers

5.3.2.1 FATO perimeter markings or markers should be provided at a vertiport where the extent of a FATO is not self-evident as shown in Figures 16a and 16d.

5.3.2.2 For an unpaved FATO, the perimeter should be defined by flush in-ground markers.

5.3.2.3 For a paved FATO, the perimeter should be defined with a painted dashed line.

5.3.2.4 The FATO perimeter marking, or markers should have the following characteristics:

a. be located on the edge of the FATO

b. be 30 cm in width, and 1.5 m in length, as shown in Figure 13

c. have end-to-end spacing of not less than 1.5 m and not more than 2 m with corners of a square or rectangular FATO defined

d. coloured white.

## 5.3.3 TLOF perimeter marking

5.3.3.1 A TLOF perimeter marking should be displayed if the perimeter of the TLOF is not selfevident, as shown in Figures 16a to 16d.

5.3.3.2 A TLOF perimeter marking should be located along the edge of the TLOF.

5.3.3.3 A TLOF perimeter marking should consist of a continuous white line with a width of 30 cm.

## 5.3.4 Touchdown positioning marking (TDPM)

![07df428e165e3b8fb8a7d10c2d542f1df23cc97c1a25f4002f6229ed6aad4be0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/07df428e165e3b8fb8a7d10c2d542f1df23cc97c1a25f4002f6229ed6aad4be0.jpg)  
Figure 14 – Touchdown positioning circle marking

5.3.4.1 A TDPM should be provided where a VCA is to touchdown or be accurately placed in a specific position, as shown in Figures 16a to 16d.

5.3.4.2 The TDPM should be:

a. when there is no limitation on the direction of touchdown/positioning, a touchdown/positioning circle (TDPC) marking

b. when there is a limitation on the direction of touchdown/positioning a single shoulder line with an associated centreline

c. be a yellow line with a width of at least 0.5 m.

5.3.4.3 The TDPM should have the following characteristics:

a. the inner edge/inner circumference of the TDPM should be at 0.25 Design D from the centre of the area in which the VCA is to be positioned

b. when a shoulder line, the length of the marking should be 0.5 Design D

c. be a yellow line with a width of at least 0.5 m.

5.3.4.4 The TDPM should be the primary marking when used in conjunction with other markings on the TLOF.

## 5.3.5 Aiming point marking

![342e61f40b83fdb17bd3a6f297b9d71f8b9a5e0c5ea7cce3ec440367dd96788d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/342e61f40b83fdb17bd3a6f297b9d71f8b9a5e0c5ea7cce3ec440367dd96788d.jpg)  
Figure 15 – Aiming point marking

5.3.5.1 An aiming point marking should be provided at a vertiport where it is necessary for a pilot to make an approach to a particular point above a FATO before proceeding to a TLOF,

as shown in Figure 16c. The aiming point marking should be located at the centre of the FATO.

5.3.5.2 The aiming point marking should be located at the centre of the FATO

5.3.5.3 The aiming point marking should have the following characteristics:

a. be an equilateral triangle with the bisector of one of the angles aligned with the preferred landing direction

b. consist of continuous lines

c. the dimensions of the marking should conform to those shown in Figure 15.

## 5.3.6 Vertiport identification marking

5.3.6.1 A vertiport identification marking may be provided within a FATO, as shown in Figures 16a, 16b and 16d.

5.3.6.2 Where a TDPC is provided, the vertiport identification marking should be in the centre of the TDPC. Otherwise, the vertiport identification marking should be located at or near the centre of the FATO.

5.3.6.3 A vertiport identification marking should have the following characteristics:

a. a form that identifies the vertiport

b. have colour(s) that do not conflict with or detract from the TDPC where used

c. have a size that not less than 3 m and not greater than 0.5 Design D in its longest dimension

d. have a form that allows the marking to be aligned with the preferred landing direction.

5.3.6.4 The use of the letter "H" and "X" should be avoided as to not conflict with the heliport identification marking and an unserviceability marking. Markings with a white cross should also be avoided.

Note: The vertiport identification marking need not be limited to a single form for all vertiports, however the marking used should be consistent across a facility. For example, a vertiport operator may choose to use a vertiport identification marking defined by another aviation authority, or they may choose to use a corporate logo or brand that aligns with the characteristics in 5.3.5.3.

5.3.6.5 Where a vertiport is equipped with two or more FATOs, vertiport identification markings may be supplemented or replaced with an ordinal number marking, as shown in Figure 16d.

5.3.6.6 An ordinal number marking should consist of the following characteristics:

a. arranged as to be readable from the preferred landing direction

b. a number, beginning with 1 and ending in the last of the numbered FATOs

c. have a colour consistent with the vertiport identification marking

d. have a size not less than 1.5 m and not greater than 0.5 Design D in its longest dimension.

## 5.3.7 Vertiport name marking

5.3.7.1 A vertiport name marking may be provided at a vertiport, as shown in Figure 16d.

5.3.7.2 A vertiport name marking should consist of the name or the alphanumeric designator of the vertiport.

5.3.7.3 A vertiport name marking intended for use at night should be illuminated, either internally or externally.

5.3.7.4 The characters of the marking should be not greater than 1.2 m in height.

## 5.3.8 Maximum allowable weight marking

5.3.8.1 A maximum allowable weight marking may be displayed to provide the weight limitation of the TLOF, as shown in Figures 16a and 16d.

5.3.8.2 A maximum allowable weight marking should be located within the TLOF.

5.3.8.3 A maximum allowable weight marking should consist of a one-, two- or three-digit number.

5.3.8.4 The maximum allowable weight should be expressed in tonnes to the nearest 100 kg. The marking should be presented to one decimal place and rounded to the nearest 100 kg followed by the letter 't'.

5.3.8.5 The maximum allowable weight marking should consist of the following characteristics:

a. arranged as to be readable from the preferred landing direction

b. have a size that not less than 0.6 m in its longest dimension.

## 5.3.9 D-Value marking

5.3.9.1 A D-value marking may be displayed to provide the pilot with the limiting D of the FATO or TLOF, as shown in Figures 16a and 16d.

5.3.9.2 A D-value marking should be located within the FATO or TLOF and so arranged as to be readable from the preferred landing direction(s).

5.3.9.3 The D-value marking should be rounded to the nearest whole metre with 0.5 rounded down.

5.3.9.4 The D-Value marking should consist of the following characteristics:

a. arranged as to be readable from the preferred landing direction

b. have a size that not less than 0.6 m in its longest dimension.

## 5.3.10 Vertiport marking examples

![9353c2548d197d806623e90eec85db96137bc7e97d91c615d9b5bcb8d1f9f8d8.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9353c2548d197d806623e90eec85db96137bc7e97d91c615d9b5bcb8d1f9f8d8.jpg)  
Figure 16a – Vertiport marking example 1

Figure 16a illustrates an example of marking a FATO on a natural surface and includes:

FATO – Natural surface. White flush markers (1.5m x 0.3m)

TLOF – Grey painted square with edge marked by continuous white line (>0.3m)

TDPM – Always an internal diameter 0.5 of Design D. Marked by a continuous yellow circle (0.5-1m wide)

vertiport identification – European Union Aviation Safety Agency (EASA) white V on a blue background

D-Value and maximum allowable weight markings.

Note: The image is an example only and does not limit possible marking combination on a natural surface.

![3600b83921007282adab358c0a125b8a07dcf69c83729d3e5151da9956b0c65c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3600b83921007282adab358c0a125b8a07dcf69c83729d3e5151da9956b0c65c.jpg)  
Figure 16b – Vertiport marking example 2

Figure 16b illustrates an example of marking a FATO on a paved surface and includes:

FATO – Light coloured paving. White markings (1.5m x 0.3m) with black outline for contrast with paving

TLOF – Green painted circle with edge marked by continuous white line (>0.3m) and a black outline for contrast with paving

TDPM – Always an internal diameter 0.5 of Design D. Marked by a continuous yellow circle (0.5-1m wide)

vertiport Identification – Federal Aviation Administration broken wheel

• 2 types of flight path alignment guidance markings.

Note: The image is an example only and does not limit possible marking combination on a paved surface.

![f815741dd4d9d885a49ef51988906aeca910be186e6735e20c6dc8cff4248055.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f815741dd4d9d885a49ef51988906aeca910be186e6735e20c6dc8cff4248055.jpg)

## Figure 16c – Vertiport marking example 3

Figure 16c illustrates an example of marking a FATO with an aiming point and stand and includes:

FATO – Natural surface. White flush markers (1.5m x 0.3m)

Air-taxi route markers – 1.5 m x 0.15 m yellow markers

TLOF – Mesh deck with edge marked by continuous white line (>0.3m)

• TDPM – Internal diameter 0.5 of Design D, marked by a continuous yellow circle (0.5-1m wide)

vertiport identification – none

flight path alignment – white arrow markings.

Note: The image is an example only and does not limit possible marking combinations.

![d97c28415a67a001f072a6bad6f6c557147e3e23e4010472457eeb01de6282df.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d97c28415a67a001f072a6bad6f6c557147e3e23e4010472457eeb01de6282df.jpg)  
Figure 16d – Vertiport marking example 4

Figure 16d illustrates an example of marking a FATO on a paved surface and includes:

FATO – Self-evident as dark paving against light concrete

• TLOF (at 1 Design D) – Painted paved octagon with edge marked by continuous white line (>0.3m.)

• TDPM – Internal diameter 0.5 of Design D marked by a continuous yellow circle (0.5-1m wide)

vertiport identification – Corporate logo with ordinal number

vertiport name marking.

Note: The image is an example only and does not limit possible marking combinations.

## 5.4 Markers and markings - taxiways and stands

## 5.4.1 VCA taxiway markings and markers

5.4.1.1 The centreline of a VCA taxiway should be marked, as shown in Figure 4.

5.4.1.2 A VCA taxiway centre line marking should be a continuous yellow line 15 cm in width.

5.4.1.3 A VCA taxiway that will not accommodate painted markings should be marked with flush in-ground yellow markers, 15-cm-wide and approximately 1.5 m in length, spaced at intervals sufficient to provide directional guidance to pilots.

## 5.4.2 VCA air taxi-route markings and markers

5.4.2.1 The centre line of a VCA air taxi-route should be marked, as shown in Figure 4.

5.4.2.2 A VCA air taxi-route centre line marking should be a continuous yellow line 15 cm in width.

5.4.2.3 A VCA air taxi-route that will not accommodate painted markings should be marked with flush in-ground 15 cm-wide and approximately 1.5 m in length yellow markers, spaced at intervals sufficient to provide directional guidance to pilots.

## 5.4.3 VCA stand markings

![b0cef5baca8d1ef8e9b68649f8b2b80dc9e1fb7a33adeed052b28131603159ab.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/b0cef5baca8d1ef8e9b68649f8b2b80dc9e1fb7a33adeed052b28131603159ab.jpg)  
Figure 17 – D-value-based stand markings

5.4.3.1 A VCA stand should be marked, as shown in Figure 17 and consist of the following elements: a. a TDPM b. a stand perimeter marking c. lead-in/lead-out markings.

5.4.3.2 VCA stand markings may also include: a. an alignment line b. a stand designation marking c. stand limitation markings d. apron safety lines.

## Touchdown positioning marking (TDPM)

5.4.3.3 A stand should be provided with the appropriate TDPM, according to 5.3.4.

## Stand perimeter marking

5.4.3.4 A VCA stand perimeter marking should consist of a continuous yellow line and have a line width of 15 cm.

5.4.3.5 When unpaved, the stand perimeter should be marked with flush in-ground markers.

## Lead-in/lead-out lines and alignment line

5.4.3.6 The TDPM, alignment lines and lead-in/lead-out lines should be located such that every part of the VCA can be contained within the VCA stand during positioning and permitted manoeuvring.

5.4.3.7 Curved portions of alignment lines and lead-in/lead-out lines should have radii appropriate to the design aircraft or the ground equipment used to position aircraft for that stand.

5.4.3.8 Alignment lines and lead-in/lead-out lines should be continuous yellow lines and have a width of 15 cm. Where it is intended that VCA proceed in one direction only, arrows indicating the direction to be followed may be added as part of the alignment lines.

## Stand designation marking

5.4.3.9 VCA stand designation markings may be provided where there is a need to identify individual stands.

5.4.3.10 A stand designation marking should consist of the following characteristics:

a. arranged as to be readable from the preferred approach direction/s

b. an ordinal designation of alphanumeric characters

c. be yellow in colour

d. have a size that not less than 0.5 m and not greater than 0.25 Design D in its longest dimension.

## Stand limitation marking

5.4.3.11 Where a stand is designed to accommodate a design aircraft with a smaller D-value, or a lesser weight than is accommodated by other vertiport facilities, the marking showing the limiting D-value or weight should be displayed on the lead-in line to that stand.

5.4.3.12 The stand limitation marking should consist of the following characteristics:

a. arranged as to be readable prior to entering the stand

b. be yellow in colour

c. have a size that not less than 0.5 m and not greater than 0.25 D in its longest dimension

d. centrally located on the lead-in line, with the lead in line broken to accommodate the marking.

5.4.3.13 A weight-based stand limitation marking should be consistent with 5.3.8.

5.4.3.14 A D-value based stand limitation marking should be consistent with 5.3.9.

## Apron safety line marking

5.4.3.15 Apron safety lines may be provided on an apron as required by the parking configurations and ground facilities.

5.4.3.16 Apron safety lines may be located to define the areas intended for use by ground vehicles and other aircraft servicing equipment, passengers and pedestrians, etc., to provide safe separation from aircraft.

5.4.3.17 Apron safety lines should have the following characteristics:

a. be of a conspicuous colour, preferably red, which should contrast with that used for VTOL-capable aircraft stand markings

b. be continuous in length and at least 10 cm in width.

## 5.5 Visual aids - Lighting

## 5.5.1 General

5.5.1.1 Lights and lighting systems should be installed, in accordance with the following specifications, at a vertiport used or available for operations at night.

5.5.1.2 The photometrics for vertiport lights and lighting elements (including light output, vertical and horizontal distribution, and chromaticity) should be appropriate to the vertiport environment and intended operations without being visually distracting or confusing to pilots.

Note: Annex 14 Volume II may be used as a starting point for vertiport designers and operators to gain an understanding of legacy heliport lighting systems and from there determine the appropriate photometrics (such as light output, vertical and horizontal distribution, and chromaticity) that will provide the safest outcome for their intended VCA operations.

However, the application of Annex 14 Volume II may not suit VCA operations or the location of a vertiport where vertical procedures are intended or the vertiport is in a community sensitive location.

5.5.1.3 If the operating environment varies, lighting systems should be adjustable in order to achieve the appropriate intensity, if needed.

## 5.5.2 Approach lighting system

Reserved

## 5.5.3 Flight path alignment guidance lighting system

![8f4dae4a9b6c21e2d390772d5331e73da8909662bf756dcb0ce5218f2f34126f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8f4dae4a9b6c21e2d390772d5331e73da8909662bf756dcb0ce5218f2f34126f.jpg)  
Note - Markings have been shaded to emphasise the lighting

Figure 18 - Flight path alignment guidance lights and arrangement for aiming point lights

5.5.3.1 Flight path alignment guidance lighting system(s) (FPAGLS) should be provided at a vertiport where it is desirable and practicable to indicate available landing and/or take-off path direction(s), as shown in Figure 18.

5.5.3.2 The flight path alignment guidance lighting system should be located in a straight line along the direction(s) of approach and/or departure path to/from the TLOF or FATO within FATO, TLOF or protection area.

5.5.3.3 If combined with a flight path alignment guidance marking, as far as is practicable the lights should be located inside the “arrow” markings.

5.5.3.4 A flight path alignment guidance lighting system should consist of the following characteristics:

a. a row of three or more lights spaced uniformly with a total minimum distance of 6 m

b. intervals between lights should not be less than 1.5 m and should not exceed 3 m

c. where space permits, there should be 5 lights

d. be steady omnidirectional inset white lights.

5.5.3.5 Where a FPAGLS is for an approach only or departure only (but not both), additional lights can be added to indicate the desired direction. These lights should have the following characteristics:

a. a barrette of 3 lights, spaced 0.5 m apart

b. perpendicular to the line of the FPAGLS

c. located centrally between the last and second to last light to form an arrow-head.

5.5.3.6 The system should allow an adjustment of light intensity to meet the prevailing conditions and to balance the flight path alignment guidance lighting system with other vertiport lights and general lighting that may be present around the vertiport.

## 5.5.4 Visual alignment guidance system

Reserved

## 5.5.5 Visual approach slope indicator

Reserved

## 5.5.6 FATO Perimeter lights

5.5.6.1 Where a FATO is established at a vertiport for use at night, the FATO should be provided with perimeter lights

5.5.6.2 FATO perimeter lights should be placed along, outside and within 0.3 m of the edge(s) of the FATO. The lights should be uniformly spaced as follows:

a. for a straight edge, a light at the end of each edge, then with lights evenly spaced at not more than 5 m apart

b. for a curved edge, lights evenly spaced and not more than 5 m apart.

5.5.6.3 FATO perimeter lights should have the following characteristics:

a. be fixed omnidirectional lights

b. white in colour

c. be inset where the FATO and TLOF are collocated and accessed by a taxiway, otherwise, be not more than 25 cm in height.

## 5.5.7 Aiming point lights

![3c1c0fd6909466fadaa7d3e5ebe8cbb4cd0c728c89782deaad95fc59282d9d1b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3c1c0fd6909466fadaa7d3e5ebe8cbb4cd0c728c89782deaad95fc59282d9d1b.jpg)  
Figure 19 – Arrangement for aiming point lights

5.5.7.1 Where an aiming point marking is provided at a vertiport intended for use at night, aiming point lights should be provided, as shown in Figure 18 and 19.

5.5.7.2 Aiming point lights should be collocated with the aiming point marking.

5.5.7.3 Aiming point lights should form a pattern of at least six omnidirectional white lights. The lights should be inset when a light extending above the FATO could endanger VCA operations.

## 5.5.8 TLOF lighting system

5.5.8.1 Where a TLOF is established at a vertiport for use at night, the TLOF perimeter should be lit, unless the TLOF is centrally located within the FATO, the TDCP is lit, or is located within a stand lit by floodlighting, as shown in Figures 20a and 20c.

## 5.5.8.2 The lighting for the TLOF should consist of:

a. TLOF perimeter lights

and/or

b. TDPC lighting segments.

## TLOF - perimeter lights

5.5.8.3 TLOF perimeter lights should be placed along, outside and within 0.3 m of the edges of the TLOF. The lights should be uniformly spaced as follows:

a. for a straight edge, a light at the end of each edge, then with lights evenly spaced between at not more than 3 m apart

b. for a curved edge, light evenly spaced and not more than 3 m apart.

5.5.8.4 TLOF perimeter lights should have the following characteristics:

a. be fixed omnidirectional lights

b. green in colour

c. be inset where the TLOF is accessed by a taxiway, otherwise, be not more than 5 cm in height.

## TLOF - lighting segments

## Reserved

## TDPC - lighting segments

5.5.8.5 Lighting segments should have the following characteristics:

a. a width no larger than the marking it defines

b. a frame the same colour as the marking it defines

c. have a finish that does not reduce surface friction of the TLOF.

5.5.8.6 Lighting segments, where provided to identify the TDPC, as shown in Figure 20b, should have the following characteristics:

a. a total length of lighting segments, in a pattern, of between 50% and 75% of the length of the pattern

b. be evenly spaced with gaps between lighting segments of not less than 0.5 m

c. be placed within the marking designating the TDPC such that the lighting segments are within 10 cm of the inner edge of the marking

d. show yellow light.

## 5.5.9 Vertiport identification marking lighting

5.5.9.1 The vertiport identification marking may be lit.

5.5.9.2 Vertiport identification marking lighting should not adversely impact the TLOF surface.

## 5.5.10 VCA taxiway/air taxi-route lighting

5.5.10.1 Where a taxi-route is established at a vertiport for use at night, the taxi-route centreline should be lit.

5.5.10.2 Taxi-route lights should be placed along the taxiway centreline spaced at intervals sufficient to provide directional guidance to pilots.

5.5.10.3 Taxiway lighting should be yellow, and air taxi-route lighting should be alternating yellow and green, as shown in Figure 20c.

## 5.5.11 VCA stand lighting

5.5.11.1 VCA stand lighting should be provided on a stand intended to be used at night by VCA.

5.5.11.2 VCA stand lighting floodlights, as shown in Figure 20c, should be located to provide adequate illumination, with a minimum of glare to the pilot of an aircraft in flight and on the ground, and to personnel on the stand. The arrangement and aiming of floodlights should be such that a VCA stand receives light from two or more directions to minimise shadows.

5.5.11.3 The spectral distribution of stand floodlights should be such that the colours used for surface and obstacle markings can be correctly identified.

5.5.11.4 Horizontal and vertical illuminance should be sufficient to ensure that visual cues are discernible for required manoeuvring and positioning, and essential operations round the VTOL aircraft can be performed expeditiously without endangering personnel or equipment.

## 5.5.12 Vertiport lighting examples

![5fddc3593dc90f0b15f63791a83632d0145ec90e30d78811a7ac59382a06c15a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5fddc3593dc90f0b15f63791a83632d0145ec90e30d78811a7ac59382a06c15a.jpg)

## Figure 20a – Vertiport lighting example 1

Figure 20a illustrates an example of lighting a FATO that includes:

FATO - white omnidirectional lights not more than 5 m apart

TLOF - green omnidirectional perimeter lights not more than 3 m apart

TDPC - in this case not lit

flight path alignment guidance lighting - 5 white omnidirectional lights.

Note: The image is an example only and does not limit possible vertiport lighting combinations.

![48c6ee3a47050c83cd17c9cf12af7fb5cd78eac9429de949dae4deb2041da638.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/48c6ee3a47050c83cd17c9cf12af7fb5cd78eac9429de949dae4deb2041da638.jpg)  
Figure 20b – Vertiport marking example 2

Figure 20b illustrates an example of lighting a FATO that includes:

• FATO - white omnidirectional lights not more than 5 m apart

TLOF - not lit as the TDPC is lit

TDPC - yellow lighting segments.

Note: The image is an example only and does not limit possible vertiport lighting combinations.

![613c4e161a8df8918391c7f73d38b044ee71fc9a001baf0e75404037a10ad9d3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/613c4e161a8df8918391c7f73d38b044ee71fc9a001baf0e75404037a10ad9d3.jpg)  
Figure 20c – Vertiport marking example 3

Figure 20c illustrates an example of lighting a FATO and stand that includes:

aiming point with 6 white omnidirectional lights

• FATO white omnidirectional lights evenly spaced not more than 5 m apart

flight path alignment guidance lights of 5 white omnidirectional lights

air-taxi route markers – yellow/green alternating omnidirectional lights

stand TLOF & TDPM – stand floodlights

vertiport identification is not lit.

Note: The image is an example only and does not limit possible vertiport lighting combinations.

## 5.6 Machine-readable visual aids

Nothing in the specifications above preclude the use of machine-readable aids, such as QR codes, being used for aircraft or vehicle guidance on a vertiport.

# CASA Guide to Vertiport Design (2024)

Guide to vertiport design

ISBN: 978-1-76137-043-4 (PDF)

© Commonwealth of Australia 2024

![b72719ec6b415e333d965aaa954c1be47cbe50ee5730ecba896781f7ed22eab4.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/b72719ec6b415e333d965aaa954c1be47cbe50ee5730ecba896781f7ed22eab4.jpg)

With the exception of the Coat of Arms and all photos and graphics, this publication is licensed under a Creative Commons Attribution 4.0 International Licence. The Creative Commons Attribution 4.0 International Licence is a standard form licence agreement that allows you to copy, distribute, transmit and adapt this publication provided that you attribute the work.

The full licence terms are available from: www.creativecommons.org/licenses/by/4.0/.

The Civil Aviation Safety Authority asserts the right to be recognised as the author of the original material in the following manner:

The document must be attributed as the Civil Aviation Safety Authority Guide to vertiport design.

Cover image: Eve Air Mobility Inside cover image: Skyportz

2401.4820

![99fcbb345b7c86ab33f14e7d20901c86de84b6f56aabb6eebd421ac93c44a7f7.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/99fcbb345b7c86ab33f14e7d20901c86de84b6f56aabb6eebd421ac93c44a7f7.jpg)

The eVTOL aircraft images contained in this document are for illustrative purposes only and do not imply CASA or Australian Government endorsement of any particular aircraft concept or organisation. All AAM operations are subject to regulatory approvals.

![8719e17f1bff13d61afbbee4c5ffe7eee366e70af0816e24ce6c25b7a5ea9bf0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8719e17f1bff13d61afbbee4c5ffe7eee366e70af0816e24ce6c25b7a5ea9bf0.jpg)

## Contents

Introduction 3   
Who this guide is for? 4   
About this guide 5   
Advanced air mobility (AAM) – overview 5   
Vertical take-off and landing (VTOL)   
capable aircraft (VCA) 6   
Vertiports – overview 9   
Influences on vertiport design 12   
Designing a vertiport 15   
The Design VTOL-capable aircraft   
(Design VCA) concept 16   
A building block approach to   
vertiport design 18   
Obstacle limitation surfaces 24   
Visual aids 31   
Where to from here? 41   
Appendix A – Acronyms and   
initialisms 42   
Appendix B – Definitions 43

![891217e21db18d2dc53f2a2f4675f0fb5b4ba2ca7aa0a2f2fe10873dd3a4ad5d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/891217e21db18d2dc53f2a2f4675f0fb5b4ba2ca7aa0a2f2fe10873dd3a4ad5d.jpg)

## Introduction

Who this guide is for? 4   
About this guide 5   
Advanced air mobility (AAM) – overview 5   
Vertical take-off and landing (VTOL) capable aircraft (VCA) 6   
Vertiports – overview 9   
Influences on vertiport design 12

![eba931d28a45b5a0596b4dc8f379594aa7c950bd3b63110bf8986332c345eee4.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/eba931d28a45b5a0596b4dc8f379594aa7c950bd3b63110bf8986332c345eee4.jpg)

## Who this guide is for?

This guide is for:

people and organisations involved in the design, construction and operation of vertiports

• planning authorities

• aerodrome operators

• VTOL-capable aircraft operators and manufacturers.

The terms and abbreviations used in this guide are found in Appendices A and B.

![c5c05568ddec5a9eb54e30fefe35284977c57f7be3d18dc92d5a4f785b84e42f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c5c05568ddec5a9eb54e30fefe35284977c57f7be3d18dc92d5a4f785b84e42f.jpg)

## About this guide

This guide to vertiport design provides easy to understand explanations and examples to compliment the Civil Aviation Safety Authority (CASA) advisory circular AC 139.V–01 Guidance for vertiport design. It is not intended to be an exhaustive description of the specifications in the AC.

The AC, and this guide, are for the initial planning and design of vertiports intended for vertical take-off and landing (VTOL) capable aircraft (VCA) operating with a pilot on board in visual conditions only. The following operations are not covered by this guidance:

flights in instrument flight conditions (where the conditions are not good enough for the pilot to use outside visual references)

flights operating under digital flight rules (as proposed by NASA)

• flights operating with any form of autonomy.

AC 139.V–01 is largely based on experience with helicopter operations. At the time of publication, no VCA have been certified by any country and it is not possible to be certain that the capabilities of future VCA will match those of currently certified helicopters.

Guidance on vertiport operations, maintenance, serviceability, emergency response, as well as safety and risk management systems, are in development. They are not included in this guide.

As the industry evolves, new guidance will be produced and current guidance will be updated. Please keep in touch at the CASA website:

## Advanced air mobility (AAM) – overview

Advanced air mobility (AAM) is the term used to describe an evolving aviation transport ecosystem, based on new and emerging aircraft types incorporating the following advances in technology:

• lightweight and powerful electric motors

high power, yet light weight, battery systems with longer endurance

• distributed electrical propulsion

• hydrogen fuel cell and hybrid power systems

fly-by-light (fibre-optic data transfer) control systems

• low noise profile designs.

These technologies are enabling small start-up companies to compete with large aircraft manufacturers to design AAM aircraft. The aircraft will probably be produced and operated at lower costs than legacy hydrocarbon fuelled aircraft.

We envisage that a variety of aircraft will suit a range of missions including:

• urban air mobility:

– inner-city rooftop-to-rooftop air taxis

– city to airport transfers

• regional air mobility:

– linking regional towns and cities.

## Vertical take‑off and landing (VTOL) capable aircraft (VCA)

Vertical take-off and landing (VTOL) capable aircraft (VCA) are heavier-than-air aircraft capable of vertical take-off or landing procedures by means of more than two thrust units. VCA do not include aeroplanes or helicopters.

Note: A vertical take‑off or landing may also include a horizontal component.

VCA designs are many and varied, with the Vertical Flight Society (VFS) listing over 800 concepts on their website (https://evtol.news/aircraft).

There are organisations that track VCA as they progress through development, testing and towards the delivery of a certified product at a commercial scale. Their statistics indicate that the number and variety of VCA that progress from concept to successful certification will be an important consideration for prospective vertiport operators.

![6faa000bf680bd35f3b8fc66d8c0e1021de9b0a151cda13074ea72e39b4f3373.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6faa000bf680bd35f3b8fc66d8c0e1021de9b0a151cda13074ea72e39b4f3373.jpg)

The advanced air mobility reality index, aamrealityindex.com, is a tracking tool which is based on a propriety formula that uses publicly available information and expert knowledge. It helps assess an industry entrants’ progress toward the delivery of a certified product at commercial scale.

Components of a vertiport will need to be designed to accommodate the VCA that will operate from it. This is covered in detail later in this guide.

Figure 1 provides an overview of different aircraft types, including conventional aircraft and VCA, as well as their possible sources of power and propulsion systems. Aircraft types addressed by this guide are colour coded yellow.

Figure 1: Aircraft and powertrain classifications  
![16171c166acbdd9af001eace0a29428ee4d4f03ff36ccf4fd49dd356bcc19a2c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/16171c166acbdd9af001eace0a29428ee4d4f03ff36ccf4fd49dd356bcc19a2c.jpg)

## Multicopter (pure lift)

A multicopter is a VTOL-capable aircraft (VCA) with more than two lift-generating propulsors and with no fixed-wing surface for horizontal flight.

Current discussion within the AAM industry has suggested that a multicopter should be labelled as an axicraft. The rationale is based on the way lift is only generated along the propulsor axis (axial thrust). This is different from rotorcraft (helicopters or gyrocopters), where lift produced by the rotor can be tilted to direct thrust along, and off, its spin axis.

Figure 2: Thrust control: axial thrust propulsors versus rotor  
![f66c81661d4684f7d952ef3a9e5a7663b3f23bac34b994b0e9e10e86d4448de0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f66c81661d4684f7d952ef3a9e5a7663b3f23bac34b994b0e9e10e86d4448de0.jpg)  
Examples of multicopter VCA are the eHang EH216-S and the Volocopter VoloCity.

Figure 3: VoloCity Volocopter (image www.volocopter.com)  
![3337d0a67ccd59c880afb5925b4b2a947ab234974627036a7ecbb5334a2be7ec.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/3337d0a67ccd59c880afb5925b4b2a947ab234974627036a7ecbb5334a2be7ec.jpg)

## Lift plus (+) cruise

Lift plus (+) cruise VCA have a set of propulsors for generating lift for vertical flight and an additional set of propulsors combined with a fixed-wing surface for cruising in horizontal flight. It is a popular VCA design concept as there is no need for complex titling mechanisms for vectored thrust. Having a fixed wing for cruise provides better range than can be achieved by a pure multicopter. Examples of lift + cruise VCA are the Wisk Generation 5 (Cora), Eve Air Mobility’s EVE-100 and Beta’s ALIA-250. Below is the CASA reference VCA – an example of a fictitious lift + cruise VCA.

Figure 4: Example of a lift + cruise VCA  
![acbc7f0a4e755aa7a60ec7b16141e80945991c40539d7cfb7c07741c6c642339.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/acbc7f0a4e755aa7a60ec7b16141e80945991c40539d7cfb7c07741c6c642339.jpg)

## Vectored thrust

Vectored thrust VCA have propulsors that can change the direction of thrust during flight, enabling a transition from vertical to horizontal flight. The thrust propulsors provide thrust for both lift and for cruise, either by having the propulsors themselves tilt or by having the wing (with propulsors attached) tilt. Examples of vectored thrust VCA are the Joby S4 and AMSL Aero’s Vertiia.

Figure 5: Joby S4 (image www.jobyaviation.com)  
![54631b27fef40599cc99e935e8502135653083cfed574fecc5a29ff25be3a728.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/54631b27fef40599cc99e935e8502135653083cfed574fecc5a29ff25be3a728.jpg)

There is technically a subcategory of vectored thrust that is a lift (axial thrust) plus vectored thrust. This is a popular design configuration, where we see a high winged aircraft with a series of tilting propulsors in front of the wing augmented, during vertical procedures, by a series of lift propulsors behind the wing. Examples of this lift + vectored thrust configuration are the Vertical Aerospace VX–4, Wisk Gen 6 and Archers Midnight.

Figure 6: Vertical VX–4 (image www.avweb.com)  
![603492690067390c32c2810fd02aa9a5fea2cdb4969086eac3c7cfb6ff55af9c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/603492690067390c32c2810fd02aa9a5fea2cdb4969086eac3c7cfb6ff55af9c.jpg)

![a2a555123479c30bf62aa76ccba81c1155b50e842b41eec9d35833bf7ae12d6a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a2a555123479c30bf62aa76ccba81c1155b50e842b41eec9d35833bf7ae12d6a.jpg)

## Vertiports – overview

Vertiports are an important infrastructure element of the advanced air mobility (AAM) ecosystem. Existing airports and heliports will continue to be used, however, there will eventually be a requirement for new infrastructure to accommodate emerging VCA types. A vertiport is different from a heliport (which can accommodate all vertical lift aircraft) as a vertiport facility will exclude use by helicopters.

## Key driver for new infrastructure

The majority of VCA will be electrically powered and are therefore expected to generate less noise than traditional powered aircraft. The AAM industry wants to operate in urban areas. Typically in these areas, the construction of a heliport would not be accepted by the public, due to the noise associated with helicopter operations. Lower noise VCA present a viable alternative option, thus the requirement for vertiports.

## Location

Some vertiports may be situated in large open areas that can accommodate runway-type final approach and take-off areas (FATOs). Others will be situated on small sites within a congested urban environment that are inaccessible to traditional fixed wing aircraft. These areas are where VCA can demonstrate their unique benefits and advantages.

## Size

The size of a vertiport will need to suit the VCA types that will operate from it. Sizes will vary from small vertiports, with space for one aircraft and minimal infrastructure (vertistops), to large vertiports with infrastructure that can accommodate multiple aircraft. These vertiports would have facilities to accommodate larger passenger numbers and freight, with some large enough to offer maintenance and storage facilities for fleets of aircraft (vertihubs).

Figure 7: Vertiport located at a freight handling facility  
![93318c71278b92dc2ca7b3b2f9b61aef5fa5042a019386d927e8e336d04a910c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/93318c71278b92dc2ca7b3b2f9b61aef5fa5042a019386d927e8e336d04a910c.jpg)

## Why do we need vertiport specifications when we already have heliport standards?

Vertiport specifications provide a clear separation between building a facility for all vertical lift aircraft (a heliport) and a facility that excludes helicopters (a vertiport).

This will give the AAM industry an opportunity to demonstrate to the community that a vertiport (catering only for VCA) may be more desirable than a heliport. If communities are going to accept AAM as an industry, then gaining this ‘social licence’ is vitally important. With the guidance for vertiports clearly excluding the use of helicopters then we hope that local councils and communities will be more accepting to AAM in their localities.

Also, vertiports are unlikely to cater for conventionally fuelled aircraft (for example, jet fuel or Avgas) and may not require liquid fuelling facilities or liquid fuel fire-fighting equipment. The International Civil Aviation Organization’s (ICAO) guidance for heliports (ICAO Doc 9261) recommends operators have access to firefighting foam, with quantities proportional to the size and complexity of their operation. The guidance also includes suggested deck designs which allow for safe drainage of liquid fuel from the surface. This is known as a passive fire-retarding system. Current research suggests foam and passive fire-retarding decks may be ineffective against lithium battery fires. Instead, vertiports will more likely need to be able to deliver high quantities of water for an extended period to cool runaway batteries. Future guidance will cover emergency response requirements for vertiports.

Table 1: Heliports versus vertiports
<table><tr><td colspan="2">Heliports</td></tr><tr><td>perceived as noisy</td><td>expected to be quieter</td></tr><tr><td>hydrocarbon-fuelled aircraft often have fuelling facilities so need to meet the requirements to contain and fight</td><td>unlikely to cater for hydrocarbon-fuelled aircraft so won&#x27;t need to consider such fire-retarding systems a hydrocarbon-based liquid fuel fire – for likely to need to provide large quantities</td></tr><tr><td>existing stigma of undesirable noise, which is not welcome in the community</td><td>runaway batteries VCA operators and manufacturers will need to demonstrate that VCA may be more desirable in the community</td></tr></table>

## Combined vertiports/heliports

If VTOL-capable aircraft (VCA) and helicopter operations are required at a single facility, the facility would need to comply with both heliport and vertiport specifications.

## Vertiport site selection – considerations

Vertiport operators will need to consider many factors, including those that are outside CASA’s remit. CASA may only provide guidance on aviation safety matters, so vertiport operators will need to reach out to many other agencies and entities to cover all the different considerations. The following table shows sample considerations and suggested agencies to contact.

Table 2: Considerations for vertiport operators, and the relevant agencies

## Sample considerations for vertiport operators

CASA

Airservices

Department of Infrastructure

Department of Environment

Home Affairs

Australian Communications and Media Authority

Bureau of Meteorology

Vertiport operator

State & local governments

Aviation safety – vertiport design, VCA certification, pilot licensing

Airspace and traffic management, published information

Aircraft noise certificates

Wildlife habitats, migratory path impacts

Physical and cyber security, screening

Communication & data – approvals, bandwidths & infrastructure

Weather recording and reporting

Land use planning approval (including noise and environmental impacts), zoning, existing transport networks, community impact and acceptance, emergency response

Vertiport concept (agnostic or bespoke ), design, layout, energy storage, local community engagement, emergency response, ground handling, OLS design and monitoring

## Influences on vertiport design

## Aircraft type

The types of aircraft that will operate from the vertiport will be one of the most important considerations in influencing vertiport design. Many of the design considerations (for example size, surface, layout) will be determined by the VCA design type (Design VCA), a concept described in detail later in this publication. A vertiport design that supports all VCA types would be an optimal approach.

## VCA power source

## Figure 9: A VCA parked at a vertistop being charged

![11c4b49822f08257ddb75cd516eca5d246f0078c032be3f47c100d3190cebe7d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/11c4b49822f08257ddb75cd516eca5d246f0078c032be3f47c100d3190cebe7d.jpg)

VCA power sources will influence different aspects of vertiport design. These include:

power grid impact and peak power availability

under apron, or on apron services, for on-stand charging or fuelling

storage area design and location for battery swapping vehicles

hydrogen fuel storage requirements

emergency response equipment – for example, roof top hydrants.

![026b2b8081ce3ce334b89d5ce47fa25dff5143379dcb2a36194120c4f870c24d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/026b2b8081ce3ce334b89d5ce47fa25dff5143379dcb2a36194120c4f870c24d.jpg)

CASA will provide guidance on considerations for emergency response in future guidance material.

## VCA manufacturer information

VCA manufacturers and operators should be an integral part of the discussion regarding the design of a vertiport. Manufacturers and operators should share the following information:

aircraft performance capabilities and limitations

aircraft dimensions and specifications

flight characteristics

how an aircraft handles in turbulence, inclement weather and crosswinds

g-loading and passenger comfort during landing, take-off and taxi

downwash and outwash modelling

## equipment requirements

types of aircraft power cell – for example, battery, hydrogen or hybrid

recharging facilities and methods – for example, battery swaps versus on-aircraft charging

emergency response requirements

ground service equipment – for example, steps, tugs or other towing devices

## maintenance of VCA

facilities for scheduled and unscheduled maintenance

the location of service centres and their proximity to the vertiport if not on site.

## Downwash and outwash considerations

A potential hazard for vertiport operations will be the downwash and outwash from VCA operating in and out of the vertiports. Currently, there is limited operational information on VCA downwash and outwash characteristics. Vertiport operators and designers will need to work closely with VCA operators, manufacturers or other sources of research to obtain this technical data. VCA manufacturers will probably publish downwash and outwash data similar to that available to airport designers when they assess jet blast areas.

Figure 10: Concept of possible downwash and outwash data  
![8c844e1e21bcb6698dea9c96029f25c7260480cae2a24a283ef2e6994ff881a9.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8c844e1e21bcb6698dea9c96029f25c7260480cae2a24a283ef2e6994ff881a9.jpg)

![5e87ce1fd57a471ae710aeb36b28d4029bab09a7d655c0e00134eed202c4a233.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5e87ce1fd57a471ae710aeb36b28d4029bab09a7d655c0e00134eed202c4a233.jpg)

Vertiport operators and designers should assess the risk of possible injury or damage due to downwash, outwash and turbulence. This may include effects on locations under or near the approach and departure paths, both within and outside the boundary of the vertiport. Risks include:

injury to vertiport staff, passengers and the public

damage to other aircraft operating or parked at the vertiport

damage to buildings and structures

damage to vehicles

damage to equipment and utilities.

Localised downwash and outwash characteristics at a vertiport will be determined by local operational experience. Warning notices should be posted in appropriate locations to inform and warn of the dangers.

## Downwash protection zone

A recent version of the Heliport Manual by ICAO includes a new section that focuses on the hazards of downwash and outwash. It has introduced the concept of a downwash protection zone. This area is specifically designed for the protection of the general public, other aircraft and those working in the vicinity of aircraft. The manual also provides new information on downwash and outwash, which quotes different caution and hazard limits for peak wind velocities.

Other systems of assessing wind comfort are also readily available online. For example, the Lawson Comfort Criteria (2001), which provides a baseline of generally acceptable wind velocities for the public.

![347d1272c80f35524cd4b27365982abe7481d3623b0d1d910d782858fb8933d1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/347d1272c80f35524cd4b27365982abe7481d3623b0d1d910d782858fb8933d1.jpg)

## Designing a vertiport

The Design VTOL-capable aircraft (Design VCA) concept 16   
A building block approach to vertiport design 17   
Obstacle limitation surfaces 24   
Visual aids 31

## The Design VTOL-capable aircraft (Design VCA) concept

Before considering the details of vertiport design, it is essential to understand the concept of a Design VTOL-capable aircraft (a Design VCA) as it influences the dimensions for the physical infrastructure and airspace above and around the vertiport. The Design VCA is an imaginary aircraft that embodies the critical characteristics of every aircraft that will operate at the vertiport.

## Suggested parameters for the Design VCA

The Design VCA should incorporate the characteristics of all the anticipated VCA that will operate at the proposed vertiport. For example:

the largest diameter (the Design D)

the highest maximum take-off weight (MTOW)

the widest undercarriage width (UCW)

the longest take-off or landing distances

the most critical obstacle avoidance criteria

the most critical downwash and outwash criteria.

Figure 11 is an example of how Design VCA parameters can be derived from the possible VCA types that will operate from the vertiport.

Figure 11: How to derive the Design VCA parameters

![cdd7d7ef61e727bdfcf4a3269cc8463ffd09f75ac9cb8edfe1ffa47ec6a59f33.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/cdd7d7ef61e727bdfcf4a3269cc8463ffd09f75ac9cb8edfe1ffa47ec6a59f33.jpg)

![8b5012dbe9c232e5979ca18c9e3a5cdba28c7fa7a7e6e0e27f6568d9f1869a16.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8b5012dbe9c232e5979ca18c9e3a5cdba28c7fa7a7e6e0e27f6568d9f1869a16.jpg)

The diagram above is only an example of some of the parameters to be considered when formulating Design VCA specifications. Other criteria will also need to be considered and there can be more than one Design VCA for different facilities within a single vertiport.

## Implementing the Design VCA

The example vertiport in Figure 12 demonstrates how to allow for two different Design VCA at one location.

The example has two terminals, each operating a specific VTOL aircraft. The vertiport has a single final approach and take-off (FATO) area that has been built using a Design D of 12 meters, as the Design VCA for the FATO area should have the most critical (largest) Design D of the two VCA.

Figure 12: Example vertiport design using two Design VCA  
![c6333ddd6c993f5ade7a356610883fc8521a6d9ffaf7f4683ae04e2506ca2546.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c6333ddd6c993f5ade7a356610883fc8521a6d9ffaf7f4683ae04e2506ca2546.jpg)

The taxi-routes and the stands leading to the VCA1 terminal have been built with a D-value based on a Design D of 10 m (from the Design VCA) and the characteristics of VCA1.

On the other side of the vertiport, the taxiways and stands leading to the VCA2 terminal are built with a D-value based on a Design D of 12 m and characteristics of VCA 2.

![f1f0dc1fd5fd13bd3d1e071cc350544af484caaa8468b6a402d3506e017ae5f3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f1f0dc1fd5fd13bd3d1e071cc350544af484caaa8468b6a402d3506e017ae5f3.jpg)

The term D-value is used for the dimension of a facility. For example, the D-value for size of a FATO (as specified in the AC) is 1.5 x Design D of the largest VCA.

## Future-proofing the vertiport design

Future-proofing the vertiport design could prove challenging as the initial Design VCA used in a particular vertiport project may be different to the aircraft that operate in 5 to 10 years’ time. The risk is our inability to foresee the long-term operational model for vertiports and the future aircraft types that will operate from them. This might mean needing to restrict operations or needing to completely redesign and rebuild the vertiport so it can accommodate the new VCA types.

The introduction of the Airbus A380 is a good example: many airports around the world had to redesign aprons, taxiways and runways for an aircraft type that was significantly larger and heavier than anything envisaged when the airports were designed and built.

## A building block approach to vertiport design

The concept of advanced air mobility (AAM) relies on an ecosystem of many landing sites that vary in location and design. This will range from a major vertiport with multiple stands and FATO areas, to a single pad vertistop in a semirural location. As such, the guidance for their design also needs to be flexible. CASA has taken the approach of looking at each of the vertiport physical components as building blocks consisting of essential and optional components.

## Essential vertiport components

Regardless of size, a vertiport should have at least one final approach and take-off area (FATO) and one touchdown lift-off area (TLOF).

Figure 13: Basic dimensions of the FATO and TLOF  
![86c34994d5e228356dee5559e9405257076da4de6683496cb5751914dbf009c7.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/86c34994d5e228356dee5559e9405257076da4de6683496cb5751914dbf009c7.jpg)

## Final approach and take‑off area (FATO)

The FATO has two main purposes:

to provide a visual reference of the vertiport from the air

to provide an area of containment for a VTOL-capable aircraft (VCA) in the event of a deviation, such as a rejected take-off.

The dimensions of the vertiport’s FATO will be determined by the aircraft types that it needs to support. Using the Design VCA, the length and width of the FATO will be either:

1.5 times the Design D

the distance that has been specified in the aircraft flight manual for the VCA to conduct a rejected take-off (the rejected take-off distance required).

## Solid FATO

The FATO should be solid. This is to ensure that, in the event of a critical failure during take-off, the landing of the VCA will be contained and supported until the VCA stops.

Current heliport guidance allows for a FATO to be non-solid. This is supported by many years of helicopter performance data and an understanding of their capabilities under certain circumstances. This includes helicopters operating with one engine inoperative and auto rotation capabilities. No such historical operational information is available for VCA.

Future guidance materials may allow non-solid FATOs or have smaller FATO size requirements if:

VCA are certified and shown to be able to continue safe flight and landing (in the event of a critical failure)

their required distance during a rejected take-off is less than the current FATO specifications cater for.

Figure 14: FATO size versus rejected take‑off distance requirements  
![70eb320e29398bc8df3634d287fbe4433a4f5451698d98c084e9617dba5039b0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/70eb320e29398bc8df3634d287fbe4433a4f5451698d98c084e9617dba5039b0.jpg)

![f8e5da9c24fc73176da11c0f4baff0400a4a24552087d9892a59f52b7aa82c6f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f8e5da9c24fc73176da11c0f4baff0400a4a24552087d9892a59f52b7aa82c6f.jpg)  
RTODRV – rejected take-off distance required (VCA)

Like a runway, a FATO may only be occupied by one aircraft at a time. Once occupied, the FATO is not available for landing or take-off by another VCA until the first aircraft is clear of the FATO protection area.

The FATO should be free of all but essential objects, such as visual aids (lights) or emergency equipment like in-deck firefighting nozzles. These items should not be higher than 5 cm above the FATO unless the TLOF is accessed by a taxiway; then they should be flush mounted.

## Elongated FATOs

A FATO size is sometimes determined by the rejected take-off distance required. This means that the length of the FATO sometimes needs to be greater than 1.5 times the Design D. The vertiport may operate many VCA, but if one of the VCA requires a FATO longer than 1.5 of its D, then this will be the VCA that determines the FATO length.

Figure 15: An elongated FATO  
![f65260d774990d8d1445b029cfca06fce74fe0ef81c744f323d689143ef24569.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/f65260d774990d8d1445b029cfca06fce74fe0ef81c744f323d689143ef24569.jpg)

In the above fictitious example, the VCA has a rejected take-off distance that requires a FATO length greater than twice its width. These departure directions are bi-directional in opposite directions. If the departures were omnidirectional, then the FATO would need to be larger or there would need to be additional operational procedures and restrictions.

## Touchdown and lift-off area (TLOF)

The touchdown and lift-off area (TLOF) is required to provide a safe touchdown location for VCA. This may be within the FATO or a stand. (A stand is a location within a vertiport where an aircraft can be parked, passengers can embark and disembark, or maintenance can be performed.)

The main purpose of a TLOF is to contain the VCA undercarriage. The minimum dimensions of a TLOF should be 0.83 times the Design D. This is derived from heliport recommendations which are based on the study of helicopter designs.

Figure 16: Minimum and oversized touchdown and lift-off area (TLOF)  
![37eed52fb857cf868b39b0a3973f169e756cbf166754bf395e8ba6c7eaf9994e.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/37eed52fb857cf868b39b0a3973f169e756cbf166754bf395e8ba6c7eaf9994e.jpg)  
Illustration only, not all recommended markings shown

Based on the current understanding of VCA designs, this minimum dimension will accommodate the undercarriage of the majority of VCA currently in development. If a size larger than 0.83 times the Design D is required, vertiport operators can have an oversized TLOF. There are no upper size constraints other than cost and space availability.

The TLOF should be completely free of obstacles regardless of size.

## FATO protection area (FPA)

The FATO protection area (FPA) is an area extending beyond the FATO set aside to ensure that there are no obstacles encroaching the FATO.

For heliports, this is known as the safety area. However, for vertiports, it has been decided to move away from this terminology due to potential confusion with general health and safety requirements. FATO protection areas are covered in more detail later in this guide.

## Vertiport movement areas

Vertiport movement areas are prepared for the ground movement of VCA or VCA ground handling equipment such as tugs. They include:

the final approach and take-off area (FATO)

the touchdown and lift-off area (TLOF)

taxiways

aprons.

Movement area surfaces should:

be free of obstacles, including transient (for example, wind-blown) debris

have sufficient strength for the expected static (parked vehicle) and dynamic (emergency landing) loads

be smooth and free of irregularities (lumps and bumps)

provide enough friction to ensure aircraft and vehicles have good grip and braking performance

be resistant to downwash and outwash effects from VCA

have a shape or contour to ensure effective drainage while still ensuring the safe control and stability of VCA when touching down, lifting off or manoeuvring generally

not have a surface slope exceeding 2% (longitudinal slopes on a taxiway may be not more than 3%).

Figure 17: Vertiport taxiway clearance dimensions  
![c757b1e64a4e8623b4c5fe29101f6bb68feda6bd235b6f7d2ff69fe20636bb1d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/c757b1e64a4e8623b4c5fe29101f6bb68feda6bd235b6f7d2ff69fe20636bb1d.jpg)

## Optional vertiport components

## Taxiways

Vertiport taxiways allow VCA to taxi under their own power or to be towed. Taxiway dimensions are based on the width of the widest VCA undercarriage that will be operated from the vertiport. In cases where large vehicles and other pieces of ground servicing equipment are to be used, these dimensions will also need to be considered. Clearance distances between VCA on the taxiways and objects, for example parked aircraft, are also an important design consideration:

Taxiways should be at least two times the undercarriage width of the Design VCA.

The distance between a VCA and an object should be at least 0.25 times the maximum width of the Design VCA.

The distance between the wingtips of two VCA should be at least 0.25 times the maximum width of the Design VCA.

Figure 17 below demonstrates required taxiway clearances.

![1a612777c2ecb47af757f4728f178e2c86c9f861d5bdf0ec0646bcd7553a936c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/1a612777c2ecb47af757f4728f178e2c86c9f861d5bdf0ec0646bcd7553a936c.jpg)

## Taxi-routes

A taxi-route is the protected area surrounding a taxiway and is a buffer area for VCA taxiing on the taxiway. It is the equivalent to a taxiway strip at a conventional aerodrome.

There are two types of taxi-routes:
<table><tr><td>Type</td><td>Purpose</td><td>Width</td></tr><tr><td>Ground taxi-</td><td>provide protection</td><td>1.5 times the maximum</td></tr><tr><td>routes</td><td>for taxiways that only / accommodate</td><td>width of the</td></tr><tr><td></td><td>ground taxing VCA and ground d vehicles</td><td>Design VCA</td></tr><tr><td>Air taxi- routes</td><td>provide protection</td><td>2 times the</td></tr><tr><td></td><td>for taxiways that</td><td>maximum</td></tr><tr><td></td><td>accommodate air</td><td>width of the</td></tr><tr><td></td><td>taxi operations</td><td>Design VCA</td></tr></table>

Note: For taxiway dimensions, maximum width is used. This is not necessarily equal to the D.

Figure 18: Taxi-route and taxiway dimensions  
Air taxi-route = 2 x overall width  
![99ef9e263c8639bfd784f750a58e76015a5be89708ef7e4bc060b806f607ee31.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/99ef9e263c8639bfd784f750a58e76015a5be89708ef7e4bc060b806f607ee31.jpg)  
For vertiports accommodating air taxi operations (airborne taxiing of a VCA), air taxi-routes will need to be wider than ground taxi-routes to allow for the potential sideways movement of the VCA.

Air taxiing of helicopters is conducted at a height of not more than two times D above the ground at a speed of less than 20 knots. It is expected that VCA air taxiing will have similar flight performance requirements.

The ground beneath an air taxi-route may be an actual taxiway, or it may be another surface. In both cases it should be:

resistant to downwash and outwash effects

free of non-essential objects

a surface on which a VCA can conduct a forced landing.

## Stands

Stands are areas that may be provided to permit the safe loading and off-loading of passengers and cargo, as well as the servicing of the VCA, without interfering with other traffic.

Stands should all:

provide a space to safely conduct turn-around operations

be free of obstacles

have sufficient strength to support the VCA, ground servicing equipment and personnel

• be free of irregularities (i.e. should be smooth)

have a surface with sufficient friction to prevent skidding or slipping

be designed to ensure it is safe for the personnel working around the aircraft and for the passengers embarking and disembarking the aircraft.

There are two ways to design stands for a vertiport:

stands based on the heliport concept using the value of Design D (D-value stands)

stands based on the geometry of the aircraft, like at traditional airports (geometry-based stands).

Figure 19: D-value based stands and a geometry-based stand  
![de3e9e1034b19c3ec5d310904606c34d5da09e0b8e51cbfe6dedd77b80f6bd2c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/de3e9e1034b19c3ec5d310904606c34d5da09e0b8e51cbfe6dedd77b80f6bd2c.jpg)

D-value stands are the circular stands that we see at heliports. They are designed to be omnidirectional to accommodate a helicopter turning itself into the wind. On aprons with multiple stands, these will often become taxi-through type stands placed next to each other.

D-value stands require an additional protection area. This gives a larger area requirement than the geometry-based stand design. This requirement is based on a typical helicopter conducting a powered taxi to the stand, either on the ground or by air-taxi.

Geometry-based stands are limited to operations where access to the stand is by ground taxiing or by being towed onto the stand. This provides increased safety because the hazards associated with downwash and outwash are significantly reduced or eliminated when the VCA can taxi without the need to produce lift. There is also less risk of a deviation from the centreline during ground taxiing or towing.

Designing geometry-based stands requires an imaginary boundary of either 3 m or 0.25 times the maximum width of the Design VCA (whichever is greater). This should then be used to work out the space needed between stands, buildings and other objects.

![220695a5ea50778f946c8ab13b5288182b310b1134a8413d8c86f7f136865c1b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/220695a5ea50778f946c8ab13b5288182b310b1134a8413d8c86f7f136865c1b.jpg)

The 3 m or 0.25 times maximum width figures above apply to VCA with a maximum width that is less than 18 m. This covers the majority of VCA currently in development. If VCA with widths greater than 18 m are developed, then a minimum clearance distance of 4.5 m will apply.

## Obstacle limitation surfaces

A vertiport operator needs to be able to ensure that the vertiport has safe airspace that can be kept free from obstacles such as buildings, cranes or other structures. This is achieved by establishing a series of obstacle limitation surfaces (OLS) that define a volume of airspace around and above the vertiport and its surrounds.

OLS are designed to protect VCA performing visual approach-to-land or take-off procedures below 152 m above the elevation of the FATO. They comprise:

origin surfaces

approach/climb-out surfaces

transitional surfaces.

## OLS origin surfaces

OLS origin surfaces are the protection surfaces immediately around the FATO from which the rest of the surfaces are built. They include FATO protection areas, vertical protection surfaces and vertiport clearways.

The FATO protection area (FPA) is an obstacle-free space surrounding the FATO. It provides extra protection to an airborne VCA if it experiences a variation in flight path (for example, caused by a wind gust). The FPA design is based on simple geometry using FPA reference circles, circumscribed squares and common tangents:

Figure 20: FATO protection areas – reference circles, circumscribed squares and common tangents
<table><tr><td rowspan=1 colspan=1>Part</td><td rowspan=9 colspan=1>DescriptionDraw a final approach and take-off protection area(FPA) circle, centred on the FATOThe FPA reference circle has a radius of half the FATOwidth plus the greater of:•3mor0.25 Design D.If you have an elongated FATO, draw the FPAreference circle for each FATO end.</td></tr><tr><td rowspan=1 colspan=1>FPA</td></tr><tr><td rowspan=1 colspan=1>reference</td></tr><tr><td rowspan=1 colspan=1>circles</td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>Circum-</td><td></td></tr><tr><td rowspan=1 colspan=1>scribed</td><td></td></tr><tr><td rowspan=1 colspan=1>squares</td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=1 colspan=2>Common   With an elongated FATO, the protection area (FPA)tangents   needs to encompass the full length of the FATO. Thisis done by drawing direct common tangents betweenall the FATO protection area reference circles.</td></tr></table>

Building the FPA for a FATO without vertical procedures

![14222d90104e1ddbcf51cc2402b21e24a4d84e2f07423921f31607615a8ae054.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/14222d90104e1ddbcf51cc2402b21e24a4d84e2f07423921f31607615a8ae054.jpg)

![33e4cdb97473d6dce16246d9c483851d749d47ceb1abb96e3bc31b5315f928b5.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/33e4cdb97473d6dce16246d9c483851d749d47ceb1abb96e3bc31b5315f928b5.jpg)

![92fba9f1621c3f338d1946d16a88a8cca43016b775433fc91c27331c545acef2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/92fba9f1621c3f338d1946d16a88a8cca43016b775433fc91c27331c545acef2.jpg)

## Vertical procedure surface (VPS)

For a FATO that supports vertical procedures, the FATO protection area is just the reference circle. The closer the VCA is to the FATO during landing and take-off phases, the slower and more precise the movements of the VCA should be. Procedures therefore require a protection surface that increases in size as the distance from the FATO increases.

Figure 21: Building a vertical procedure surface
<table><tr><td rowspan=1 colspan=2>Part          Description</td></tr><tr><td rowspan=11 colspan=2>VPS           Draw a reference circle above andReference  centred on the FATO. The diameter ofcircle        the reference circle is determined by itsheight above the FATO.For every 100 feet above the FATO,the diameter of the VPs referencecircle increases by 1 Design D from thediameter of the FPA reference circle.For example: a VPs height of 20 feetwould mean a reference circle that is0.2 times the Design D larger than theFPA reference circle.</td></tr><tr><td rowspan=1 colspan=1>circle</td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>VPS</td><td rowspan=7 colspan=1>In the same way as for the FAToprotection area, the vertical protectionsurface will require a circumscribedsquare aligned with each flight path.This will define the inner edges of theapproach/climb-out surface and loweredges of the transitional surfaces.</td></tr><tr><td rowspan=1 colspan=1>circum-</td></tr><tr><td rowspan=1 colspan=1>scribed</td></tr><tr><td rowspan=1 colspan=1>square</td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>Obstacle</td><td rowspan=6 colspan=1>The obstacle-free volume is the spacethat is created by the truncated conethat is formed between the referencecircle of the FATO protection area (FPA)and the reference circle of the verticalprocedure surface (VPS).</td></tr><tr><td rowspan=1 colspan=1>free</td></tr><tr><td rowspan=1 colspan=1>volume</td></tr><tr><td rowspan=1 colspan=1>(OFV)</td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1></td></tr></table>

The vertical procedure surface (VPS) is an obstacle limitation surface (OLS) that is located at the height at which the VCA either begins its arriving vertical procedure, or where it ends its departing vertical procedure. This height will be determined by the performance characteristics of the most demanding VCA. For example, if one VCA has a vertical departing procedure that ends at 20 feet, and another VCA has an arriving procedure that starts at 30 feet, then the lowest, most limiting height (20 feet) is the one that needs to be protected.

![6ce03a6bda58b5dfe9ea26759e7ba5d0bf4034341391d9df74596d6dd7579628.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6ce03a6bda58b5dfe9ea26759e7ba5d0bf4034341391d9df74596d6dd7579628.jpg)

## The vertiport clearway

The next element for the vertiport obstacle limitation surfaces (OLS) is the clearway. The clearway is a protected surface that should be established where there is a need for a VCA to manoeuvre horizontally between the outer edge of either the FATO protection area (FPA) or the vertical protection surface (VPS), and the inner edge of the approach/climb-out surface.

Figure 22: Vertiport clearways  
![9bf15aed62bee442791e0c3cfbb18c1279b313e4fd482bd30a71e812a409b4dd.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9bf15aed62bee442791e0c3cfbb18c1279b313e4fd482bd30a71e812a409b4dd.jpg)  
Elevated clearway extending from the VPS

The centreline of the clearway should align with the flight path and will have a width that is not less than the width of the FATO protection area or the vertical protection surface (VPS). If the flight path between the protection area or VPS and the approach/climb-out surface needs to curve or make a change in direction, then the clearway will do the same.

It is expected that clearways will become a common feature of vertiport OLS to protect VCA as they transition from vertical to horizontal flight before continuing their initial climb out.

## Approach/climb‑out surfaces

The approach/climb-out surface consist of an inclined plane, or a series of inclined planes, or a complex surface that slopes up from inner edge of the FATO protection area (FPA) or the vertical protection surface (VPS).

Figure 23: Approach/climb-out surface  
![6e508800d4378e2fa9afb82442e83c3cd38fc7bbe33c9c6dacb917e3da27a1dd.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/6e508800d4378e2fa9afb82442e83c3cd38fc7bbe33c9c6dacb917e3da27a1dd.jpg)

Table 3: Elements of approach/climb-out surfaces
<table><tr><td>Part</td><td>Description</td></tr><tr><td>Inner edge</td><td>This should be coincident with, and equal to, the length of the edge of the circumscribed square of either the FATO protection area or the vertical protection surface (whichever has been established for the flight procedures relevant to the vertiport).</td></tr><tr><td>sides</td><td>Divergent The two sides of the surface extend from the ends of the inner edge and they diverge outwards uniformly at a rate of: 10% for day operations only 15% for day and night operations. The edges continue to splay outwards until they reach a final width of either 7 × Design D for day only operations or 10 × Design D for flightpaths to be used at night.</td></tr><tr><td>Outer edge</td><td>Once the surface reaches its final width, it will continue at that width until it reaches a final height of 152 m or 500 ft above the FATO. At that height, the surface ends at its outer edge, which will be horizontal and perpendicular to the flight path.</td></tr><tr><td>Surface slope</td><td>The upward slope of the surface is determined by the performance capabilities of the Design VCA and clearance requirements that are published by manufacturers in flight manuals. The slope or slopes will be measured in the vertical plane that contains the centreline of the approach/climb-out surface.</td></tr></table>

Notes on approach/climb-out surfaces:

CASA has not received any flight performance documentation from any manufacturer currently developing VCA. Therefore, at this stage we are not providing slope guidance for the purposes of vertiport obstacle limitation surfaces design. This will be provided when actual performance data is available.

Rather than having one set of design specifications for approach surfaces and a different set for climb-out surfaces, the specifications for the surfaces are the same.

If the flight path on approach requires a shallower angle than the reciprocal climb-out, then it is the lower flight path (the approach) that needs to be protected and it would be the approach surface that forms the obstacle limitation surface (OLS).

As with the clearway design considerations, an approach/climb-out surface is aligned with a flight path. For example, if the flight path is curved then so is the OLS.

## Transitional surfaces

The transitional surfaces provide protection parallel to the flight path from the FATO protection area (FPA) or the vertical protection surface (VPS) upwards and outwards.

The transitional surfaces protect an aircraft from obstacles if they move laterally from their intended flightpath.

Figure 24: Transitional surfaces  
![a3017882d5ee2a93a8ec1670be22e71c0ef2497190c8ba84e7d2a2c4b315ed6d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/a3017882d5ee2a93a8ec1670be22e71c0ef2497190c8ba84e7d2a2c4b315ed6d.jpg)

![33578c987dc68e4bbcb85e89972bc563e72d66e24f443eda8e8ea27478a8f601.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/33578c987dc68e4bbcb85e89972bc563e72d66e24f443eda8e8ea27478a8f601.jpg)

![61a1e588401f363088435207326762feafcca3f5f082fff4bf0ffcd10d7f5ea3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/61a1e588401f363088435207326762feafcca3f5f082fff4bf0ffcd10d7f5ea3.jpg)

Table 4: Elements of transitional surfaces
<table><tr><td>Part</td><td>Description</td></tr><tr><td>Lower edge</td><td>The lower edge of a transitional surface is drawn from the point where the approach/climb-out surface reaches its final width, then follows the edge of the approach/climb-out surface until it reaches the corner (where the splay meets the end of the inner edge). From there, the lower edge will follow the side of any clearway until it meets the vertical protection surface (VPs) or the FATO protection area (FPA). The last part of the lower edge will be along the edge of the VPs or FPA circumscribed square and any</td></tr><tr><td>Upper edge</td><td>common tangents. The upper edge also starts at the point where the approach/climb-out surface reaches its final width, but it then maintains a constant height whilst paralleling the flight path. The upper edge should end aligned with the lower edge.</td></tr></table>

Notes on transitional surfaces:

Traditionally, the transitional surface has had its own separate set of dimensions. However, because of the possible combinations of slopes, turns and final widths of the approach/climb-out surfaces, the intersection with a traditional transitional surface would be complex. CASA has, therefore, simplified the process to ensure a neat OLS design.

![5a68d9d3ecc799a178e58fc1676bde3f9f7f8c09665e2ed93a69aa3e4cbac899.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5a68d9d3ecc799a178e58fc1676bde3f9f7f8c09665e2ed93a69aa3e4cbac899.jpg)

## Complex obstacle limitation surface (OLS) designs

With the building block design methodology, vertiport operators and OLS designers will be able to construct OLS for more complex flight profiles if required.

The figures below show how a sector (or even an omnidirectional) approach can be designed by creating an arc of splays rotated around the FATO Protection Area (FPA) reference circle.LS for a sector

Figure 25: Building an OLS for a sector approach or departure  
![0405859e80c1d71629b49ba111f92918689f7cfa617f0cb3fe502af3f6b7de5c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/0405859e80c1d71629b49ba111f92918689f7cfa617f0cb3fe502af3f6b7de5c.jpg)  
The figure below shows a curved clearway. Because the transitional surface follows the edge of the clearway on the bottom edge, it should be relatively straight forward to create a transitional surface for any shaped flightpath.

Figure 26: A curved clearway from a vertical procedure surface  
![e25df93b7ea18b84d72c4ac4a1f6f6bb7364fde0686223ef6527b29b885189e3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/e25df93b7ea18b84d72c4ac4a1f6f6bb7364fde0686223ef6527b29b885189e3.jpg)

## Visual aids

In the world of aerodromes, the term ‘visual aids’ covers all the infrastructure that provides a form of information to pilots and ground operations staff around the aerodrome. These visual aids include wind indicators, ground markings and markers, lights and (on some aerodromes) movement area guidance signs.

At CASA, we tried to get a balance between outcome-based guidance and prescriptive guidance for vertiports. This is necessary for describing things like colours, shapes and patterns. We know things are going to change in this developing AAM space so we’ve tried to be flexible and to simplify the specifications wherever we could.

Advisory circular AC 139.V–01 provides details of recommended specifications for different types of visual aids. Like all the guidance in the advisory circular, the specifications are just recommendations and are not enforced by legislation. This means that a vertiport operator may choose to use other guidance material for the markers and markings, for example from the Federal Aviation Administration (FAA), the European Union Aviation Safety Agency (EASA) or ICAO. However, we hope that the guidance in the AC will give vertiport operators some flexibility in design. This will help vertiports stand out from each other visually while keeping a level of consistency so that a VCA pilot can readily identify each visual aid and its purpose.

## Wind direction indicators

Wind direction indicators are an important visual aid for a pilot to assess wind direction and strength in the vicinity of the vertiport during the critical phases of flight. Considerations for the design of a wind indicator include length, diameter, colour and colour contrast. Future technologies such as non-crewed aircraft may lead to the physical wind indicators being replaced by real-time digital weather information.

Figure 27: Wind Direction Indicators  
![aba81c970016a7c6bf55f0d0e838a3f15bd5b3248829329fe36eb05d17369ad5.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/aba81c970016a7c6bf55f0d0e838a3f15bd5b3248829329fe36eb05d17369ad5.jpg)  
Colour/s that are clearly visible against its background

## Markings and markers

The general specifications for the design of ground markings and markers have been kept very simple and outcome-based. The only general requirements are that markings and markers need to be clearly visible to the vertiport user and that they may be supplemented by reflective or refractive materials or even electroluminescent type paints if appropriate.

‘Clearly visible’ means that markings and markers need to contrast to their background or need to have a contrasting box or boundary as a background for the marking.

Markings need to be identifiable to various vertiport users, whether a pilot, operational/ ground personnel or the public.

Each marking or marker has a specific meaning or purpose:
<table><tr><td>Marker type</td><td> Meaning or purpose</td><td>Example</td><td></td></tr><tr><td>Flight path alignment guidance markings</td><td>used to show when there are defined approach and/or departure flight paths into or out from the vertiport provide important flight path information so should be the prominent marking where it overlaps with another marking, such as the FATO perimeter of TLOF</td><td></td><td><img src="images/d4217b08e68a95b4d9886fec55f2af11abca3eb761c0d8e90cbc7af266303306.jpg"/> <img src="images/15f98c37986b6fc2db616389b16017481417ca6dc65b732572f84dcc7243027a.jpg"/></td></tr><tr><td>FATO perimeter markings or markers</td><td>used to show the outer edge of the FATO the marking for the edge of a FATO is a dashed line required when the edge of the FATO is not self-evident for example when the FATO is part of a much larger concrete or asphalt surface should have contrast (consider a black background to the white dotted line) markers can be used where the surface cannot take a painted marking (such as grass) – they should be flush to the ground and resistant to downwash and outwash</td><td><img src="images/ff1db6df37e7c784574b9170915acb6a5d51ce842d463b7ebe8461add33b59e4.jpg"/></td><td></td></tr><tr><td>Marker type</td><td>Meaning or purpose</td><td></td><td></td></tr><tr><td>TLOF perimeter markings or markers</td><td>only recommended when the TLOF is not self-evident the marking for the edge of a TLOF is a solid line - otherwise same as FATO perimeter specifications</td><td>should be white</td><td><img src="images/8d3b5069a80a60e96506a5e2b8484cd8322e5140c2e53ebe4d446188bd805b00.jpg"/></td></tr><tr><td>Aiming point markings</td><td>used when a FATO is provided but where there is no TLOF if there is a preferred approach direction, this triangular marking should be aligned to that direction should be white</td><td></td><td><img src="images/5b8008764a68d080864900c62967037b57a21a07d7bc5c43b3e9bfd3fbef94d9.jpg"/></td></tr><tr><td>Touchdown positioning marking (TDPM)</td><td>the marking that the pilot uses to align and position their aircraft within the TLOF (or a stand). By positioning the pilot's seat over the touchdown positioning marking, the pilot ensures that the aircraft is correctly contained, the undercarriage is safely within the TLOF and the aircraft itself is wholly contained within the boundary of the FATO includes the touchdown positioning circle used</td><td>where touchdown direction</td><td><img src="images/ccd36299dc3444275655300b2ab4ceddf9d9e3165c094cb00c9ced8b5fd09c31.jpg"/></td></tr></table>

Vertiport identification marking

## Meaning or purpose

doesn’t have a safety purpose; more about identification. (In the future, when VCA are autonomous, the identification will mainly be for the passengers.)

needs to identify the vertiport and be readable when aligned with the preferred approach

should be centred within the touchdown positioning circle

should not be an H or an X (already used for heliport identification)

may use ordinal numbers to identify multiple FATOs within the vertiport

## Example

![ed356007416d7cf735778b1b443e7ef519b09ddae45aa0a806b1d834d511362d.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ed356007416d7cf735778b1b443e7ef519b09ddae45aa0a806b1d834d511362d.jpg)  
FAA broken wheel marking  
EASA V on blue marking

![ffcc82419b43e14ce8e38dedf59fcd850c36fc129cd35e78bba3d087df30fb75.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ffcc82419b43e14ce8e38dedf59fcd850c36fc129cd35e78bba3d087df30fb75.jpg)

![44d2615bf4676564407d6f141c7f26740da7f438bb45d4ce9758e83ca4166a67.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/44d2615bf4676564407d6f141c7f26740da7f438bb45d4ce9758e83ca4166a67.jpg)  
3 corporate marking examples

![14c62db1c2e8ca4d168ead904cbb8a900d380abfc9ba05c72a3337f332d9dac4.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/14c62db1c2e8ca4d168ead904cbb8a900d380abfc9ba05c72a3337f332d9dac4.jpg)

![07d96d381e2c6583af79e67d09c6b092228e0704912fcfc054e272749c142a96.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/07d96d381e2c6583af79e67d09c6b092228e0704912fcfc054e272749c142a96.jpg)

![e22b3a169d78e92ef42ccd932070cb3a0abcfb49349d578aa6f138079d67ef67.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/e22b3a169d78e92ef42ccd932070cb3a0abcfb49349d578aa6f138079d67ef67.jpg)

Ordinal numbering example

![b0804ba214bdd503a833b42bde7977564a19d21562478f6796eca9653c0df979.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/b0804ba214bdd503a833b42bde7977564a19d21562478f6796eca9653c0df979.jpg)

![ffc32397b594864661f748275df7b4edadafbdcefd98b0073cec825f865cad12.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ffc32397b594864661f748275df7b4edadafbdcefd98b0073cec825f865cad12.jpg)

## Taxiway and stand markings

Taxiway and stand markings provide manoeuvring guidance and are yellow in colour. The specifications for these markings have been kept consistent with traditional aerodrome (and heliport) guidance.

![d7406aea742789ae92f0e6041074373e901914cc14aff1c05c6db2b27717c97b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d7406aea742789ae92f0e6041074373e901914cc14aff1c05c6db2b27717c97b.jpg)

In general, white markings provide guidance information to the pilot for the direction of approach, acquiring the FATO area, and whether to approach to a hover (where there is an aiming point marking) or to prepare to conduct a landing. All the yellow markings take the next step and provide manoeuvring and positioning information to the pilot.

Figure 28: Stands  
![dd2de82286d8a39fca4d8af148366c4d7480c1a24935e57b2524b397df7b93f9.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/dd2de82286d8a39fca4d8af148366c4d7480c1a24935e57b2524b397df7b93f9.jpg)

<table><tr><td> Marker type Meaning or purpose</td><td></td><td></td></tr><tr><td rowspan="3">Taxiways</td><td></td><td>a continuous yellow centreline if the surface can be painted</td></tr><tr><td></td><td>in-ground, flush-mounted markers if the surface cannot be painted (for example on clay or grass surfaces)</td></tr><tr><td></td><td>where there is no physical taxiway (where there are air-taxi routes), the ground under the air-taxi route should still be marked in the same way as a physical taxiway</td></tr><tr><td>VCA stands</td><td></td><td>the most important markings are:</td></tr><tr><td rowspan="8"></td><td></td><td>a touchdown positioning marking: shoulder line type is the most common and is used where the apron design is based on a single direction parking of aircraft</td></tr><tr><td></td><td>a stand perimeter marking: provides an indication of the edge of the stand</td></tr><tr><td></td><td>perimeter where the stand is designed using the Design D lead-in/lead out markings: an extension of the taxiway centrelines leading</td></tr><tr><td></td><td>into the stand optional markings include:</td></tr><tr><td></td><td>alignment lines: assist in keeping the correct alignment for the last part of the</td></tr><tr><td></td><td>taxi onto the stand up to the parking position a stand designation and limitation markings: provide information to pilots</td></tr><tr><td></td><td>taxing into the apron. They can be used to show stand numbering or to</td></tr><tr><td></td><td>indicate where there is a limitation on the stand such as a maximum weight limit or a maximum wingspan apron safety lines: general markings used to show a safe limit of aircraft</td></tr></table>

## Other markings

Vertiport operators may also reference other guidance for providing airside visual aids. The Part 139 Manual of Standards has several other markings and visual aids that might be suitable for a vertiport such as:

pedestrian walkways (zebra crossings)

equipment storage and equipment clearance lines

apron edge lines

movement area guidance signs (MAGS).

## Vertiport lighting

CASA’s guidance on lighting in the advisory circular AC 139.V–01 is limited as our initial brief for the AC is for VCA operating in visual conditions (so lights associated only with instrument conditions were not included). However, once there is a better understanding of operations in instrument conditions, then additional lighting guidance will be added to the AC.

## Traditional lighting guidance may not be appropriate

We used outcome-based specifications for light photometrics in our guidance as traditional lighting guidance may not be appropriate.

The photometrics for vertiport lights and lighting elements (including light output, vertical and horizontal distribution, and chromaticity) should be appropriate to the vertiport environment and intended operations without being visually distracting or confusing to pilots.

Traditional aerodrome lighting guidance has been based on aerodrome environments that are typically wide-open areas outside an inner city. At night, the important lights from the perspective of a pilot approaching the airport are viewed within a void of other light. However, we expect that vertiports may be in areas where:

there will be far more light pollution around the vertiport, requiring a different or stronger light output

excess light pollution from the vertiport could cause a disturbance to nearby residents in and around residential high rises.

Also, there have been many leaps in lighting technology since aerodrome lighting specifications were written and the technology is likely to continue evolving. There could be any number of different solutions to designing an appropriate lighting system for a vertiport, and one vertiport may require a different solution to another depending on the environment within which they are located and how VCA operate to and from the vertiport.

## Different lights for different purposes

Light systems should follow a colour philosophy that matches a purpose of the lights with a particular colour.

<table><tr><td>Light colour</td><td>Purpose</td></tr><tr><td>white lights</td><td>provide initial acquisition of, and guidance to, the vertiport and include the FATO perimeter lights, the flight path alignment lights orthe aiming point lights</td></tr><tr><td>yellow lights</td><td>provide alignment guidance for touching down and alignment for taxing</td></tr><tr><td>green lights</td><td>define the TLOF or provide guidance for an aircraft air-taxiing to a TLOF</td></tr></table>

<table><tr><td>Use of light</td><td>Description</td><td>Example</td><td></td></tr><tr><td>Flight path alignment guidance lighting system (FPAGLS)</td><td rowspan="3">The FPAGLS provides an indication of available landing and take-off path directions. These are the lights that match with the alignment guidance markings and should be located within the marking as far as practicable. With the recommended minimum</td><td rowspan="3"><img src="images/bf850718b9d56ae160e5c441003f2e2c7cba747a2653df2f0cd09f7aad2d7ef8.jpg"/></td></tr><tr><td>distance between the first and last of the lights being 6 m, there will be instances where</td></tr><tr><td>FATO perimeter lights</td></tr><tr><td>Aiming point lights</td><td>pilots with a visual means to acquire the FATO while on approach to the vertiport. This system is a series of six white lights located within the white line of the triangular aiming point marking, one light</td></tr><tr><td>located at each point and one light located between each pair of corner lights. TLOF lighting systems</td><td colspan="3">There are a few options for TLOF lighting systems. The options are dependent on the locations of the TLOF. TLOFs within a FATO should by lit by green perimeter lights or yellow TDPC lighting segments, while TLOFs within a parking stand are</td></tr><tr><td>TLOF perimeter lighting</td><td colspan="3">lit by flodlighting. Green TLOF perimeter lights should be outside, but within 0.3 m of the TLOF edge. They should be spaced evenly around the TLOF not more than 3 m apart.</td></tr><tr><td>Use of light Lighting</td><td>Description</td><td>Example</td></tr><tr><td>segments and lighting elements</td><td>Lighting segments are any low-profile lighting fixture that consists of a line of lighting elements within a frame or a unit. These lighting elements could be LEDs, fibre optic cable or electro luminescent panels. There may be a single light source or there may be many. Lighting segments are used to create patterns of lights to mimic the marking they are conveying. In the case of</td><td>simplified example of a lighting segment, with three individual lighting elements. oolo 月 ≤0.1 m 0.5m</td></tr><tr><td>Lighting taxiways and taxi-routes</td><td>Guidance is outcome-based: The centreline should be lit, preferably yellow for consistency with the touchdown positioning circle to prevent confusion with the green TLOF perimeter light. The lights should be sufficiently spaced to provide guidance. Air taxi-routes could be lit with alternating green and yellow lights to help visually distinguish between a taxi-route that does not support air-taxing (ground</td><td><img src="images/6669039f7be7ca6d12fba3cd14d199c526986ab5cf8cdd2b393ed56a5d0477d7.jpg"/></td></tr><tr><td>Flood lighting for stands</td><td colspan="3">Light sources from multiple angles reduce the likelihood of having shadowed areas on the apron. Consider the horizontal and vertical components of the lighting to ensure the stand is adequately lit but that there is not a risk of glare to the pilots (or nearby</td></tr></table>

## Thinking outside the box

The lighting guidance that has been provided in the AC is generally based on historical lighting guidance for heliports as well as trying to mirror some initial guidance from a few overseas regulatory agencies. However, these historical specifications are all based on pre-existing technologies. LED technology has come a long way since there has been any update to heliport or aerodrome guidance. There is nothing in the AC that precludes a vertiport operator from looking at new technologies for lighting the vertiport so long as the specified outcomes are met.

Hypothetical examples:

## Example 1:

Paving technology proposed for roadways and paths is being developed that has integrated LEDs. Providing all the physical specifications such as strength, friction, drainage can be met, this could revolutionise how vertiports are marked and lit. This kind of ‘digital FATO’ could project its markings in real time to the FATO, the approach path and wind data could be displayed within the FATO area. Also, you could turn off FATO edge markings to indicate a FATO is occupied, and then bring up passenger markings to guide passengers to and from the terminal.

![8039ffa2d23d29d0203e1196381db125adf1b2292fccc57693e62655ac9de2f0.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8039ffa2d23d29d0203e1196381db125adf1b2292fccc57693e62655ac9de2f0.jpg)

## Example 2:

FATO information could be shared in real time with aircraft operators and aircraft in flight, allowing fine adjustment for departure, flight and arrival time to match the usage of the FATO.

## Example 3:

Future fully-autonomous aircraft may mean that markings and lights will become superfluous. Visual aids are to be seen – by a pilot. Machine readable aids such as QR codes may be used on vertiports to guide aircraft. What will a future vertiport need to be able to guide a VCA safely and accurately?

![7ef6738fe6c6ed9699bfd648f7d3c0867dd18f3f2f845037e94b5d05cd5647e1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7ef6738fe6c6ed9699bfd648f7d3c0867dd18f3f2f845037e94b5d05cd5647e1.jpg)

## Where to from here?

Advisory Circular AC139.V–01 provides greater detail of the design requirements and methods for vertiport design and should be used for actual design work.

CASA has not received (at time of publication) any flight performance documentation from any manufacturers currently developing VCA. We hope the guidance provided in the AC is specific enough to guide vertiport designers and operators in developing a safe and operationally effective facility yet open enough to promote new thinking in this evolving industry.

So, what does this mean for vertiport operators? In short, it means start talking to prospective VCA manufacturers and other stakeholders as soon as possible: the design of the vertiport may take some time.

To even start designing a vertiport, you will need to get a very good understanding of:

the sort of operations you are planning for your vertiport – both initially and in the future

• the types of VCA you want to cater for

how the flight performance of these VCA is going affect the possible flight paths

the obstacle environment that exists around your vertiport

the future development plans in the area and whether they impact the design of the vertiport.

As the industry evolves, new guidance will be produced and current guidance will be updated. Please keep in touch at the CASA emerging technologies program webpage: www.casa.gov. au/resources-and-education/publications-andresources/corporate-publications/emergingtechnologies-program.

Image: Eve Air Mobility

## Appendix A – Acronyms and initialisms

<table><tr><td>Term</td><td>Definition</td></tr><tr><td>AAM</td><td>advanced air mobility</td></tr><tr><td>AC</td><td>advisory circular</td></tr><tr><td>D</td><td>(largest) diameter (see definitions table)</td></tr><tr><td>EASA</td><td>European Union Aviation Safety Agency</td></tr><tr><td>FAA</td><td>Federal Aviation Administration</td></tr><tr><td>FATO</td><td>final approach and take-off (area)</td></tr><tr><td>FPA</td><td>FATO protection area</td></tr><tr><td>FPAGLS</td><td>flight path alignment guidance lighting system(s)</td></tr><tr><td>ICAO</td><td>International Civil Aviation Organization</td></tr><tr><td>MTOW</td><td>maximum take-off weight</td></tr><tr><td>NASA</td><td>National Aeronautics and Space Administration</td></tr><tr><td>OFV</td><td>obstacle free volume</td></tr><tr><td>OLS</td><td>obstacle limitation surface</td></tr><tr><td>RTODRV</td><td>rejected take-off distance required</td></tr><tr><td>SAF</td><td>sustainable aviation fuel</td></tr><tr><td>STOL</td><td>short take-off and landing</td></tr><tr><td>TDPC</td><td>touchdown positioning circle</td></tr><tr><td>TDPM</td><td>touchdown positioning marking</td></tr><tr><td>TLOF</td><td>touchdown lift-ff (area)</td></tr><tr><td>UCW</td><td>undercarriage width</td></tr><tr><td>VCA</td><td>VTOL-capable aircraft</td></tr><tr><td>VPS</td><td>vertical procedure surface</td></tr><tr><td>VTOL</td><td>vertical take-off and landing</td></tr></table>

## Appendix B – Definitions

<table><tr><td>Term</td><td>Definition</td></tr><tr><td>aerodrome</td><td>an area on land or water (including any buildings, installations and equipment) which is authorised under the regulations to be used as an aerodrome for the arrival, departure and movement of aircraft</td></tr><tr><td>D</td><td>for VCA: the diameter of the smallest circle enclosing the aircraft projected on a horizontal plane, while the aircraft is in the take-off or landing configuration, with lift/thrust units turning, if applicable Note: If the aircraft changes dimensions during taxing or parking (for example, folding</td></tr><tr><td>Design VCA</td><td>wings), a corresponding D(taxing) or D(parking) should also be provided a virtual aircraft type that has the largest set of dimensions, the greatest maximum take-off weight (MTOW) and the most critical obstacle avoidance criteria of the aircraft that the vertiport, or for a defined area within the vertiport, is intended</td></tr><tr><td>Design D</td><td>to serve the D of the Design VCA</td></tr><tr><td>elongated</td><td>when used with TLOF or FATO, elongated means an area which has a length more than twice its width</td></tr><tr><td>final approach and take-off area (FATO)</td><td>for the operation of a VCA, a solid area: •  from which a take-off is commenced</td></tr><tr><td>instrument meteorological conditions</td><td>• over which the final phase of approach to hover is completed means meteorological conditions other than visual meteorological conditions (see below)</td></tr><tr><td>obstacle obstacle limitation surfaces</td><td>an object (whether temporary or permanent) or part of such an object that: • is located on an area provided for the movement of aircraft • extends above a defined surface designated to protect aircraft in flight a series of planes associated with each FATO at a vertiport, which define the desirable limits to which objects or structures may project into the airspace around the vertiport so that aircraft operations at the vertiport may be conducted safely. The obstacle limitation surfaces are as follows: • FATO protection area (FPA)</td></tr><tr><td></td><td>reference circle a horizontal circle, of the specified dimension, that is centred on any intended position/flight path at or above the applicable area/surface</td></tr><tr><td>rejected take-off distance required (RTODRV)</td><td>the horizontal distance that is required from the start of the take-of to the point where the aircraft comes to a full stop, following a critical failure that is recognised at the to take-off decision point</td></tr><tr><td>touchdown and lift-off area (TLOF)</td><td>an area where a VTOL-capable aircraft may touchdown or lift off</td></tr><tr><td>touchdown positioning circle (TDPC)</td><td>a TDPM in the form of a circle, which is used for omnidirectional positioning in a TLOF</td></tr><tr><td>touchdown positioning marking (TDPM)</td><td>a marking or set of markings that provide visual cues for the directional positioning of an aircraft</td></tr><tr><td>vertical</td><td>a take-off and landing procedure that includes an initial and/or final vertical profile. The profile may or may not include a horizontal component</td></tr><tr><td>procedure vertical</td><td>a surface at which a VTOL-capable aircraft either:</td></tr><tr><td>procedure</td><td>• begins its arriving vertical procedure</td></tr><tr><td>surface (VPs) vertiport</td><td>• ends its departing vertical procedure the highest point of the FATO, or where there are multiple FATOs, the highest point</td></tr><tr><td>elevation vertiport</td><td>of the highest FATO an area of land, water or structure that is used or intended to be used for the landing, take-of and movement of VTOL-capable aircraft</td></tr><tr><td></td><td>vertiports also include vertihubs and vertistops: • vertihub: a vertiport with infrastructure for maintenance, repair, fuelling and</td></tr><tr><td></td><td></td></tr><tr><td></td><td> vertistop: a vertiport intended for take-off and landing of VCA to drop off or</td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td>parking spaces for storage of VCA</td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td>pick up passengers or cargo, but where there are no facilities for fuelling,</td></tr><tr><td></td><td>defuelling, scheduled maintenance, scheduled repairs or storage of aircraft</td></tr><tr><td></td><td></td></tr><tr><td>vertiport</td><td>a defined horizontal surface selected and/or prepared as a suitable area over</td></tr><tr><td></td><td></td></tr><tr><td>clearway</td><td>which an aircraft, capable of continued safe flight after a critical failure, may</td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td>operate between the FATO/VPS and the approach/climb-out surface inner edge</td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td></td><td></td></tr><tr><td>visual meteorological conditions</td><td>meteorological conditions expressed in terms of visibility, distance from cloud, and ceiling, equal to or better than specified minima</td></tr><tr><td>VTOL-capable aircraft (VCA)</td><td>a heavier-than-air aircraft, other than aeroplane or helicopter, capable of performing vertical procedures by means of more than two lift/thrust units</td></tr><tr><td>VCA stand</td><td>a defined area that is intended to accommodate aircraft for loading or unloading passengers, mail, or cargo, fuelling/charging, parking or maintenance</td></tr><tr><td>VCA taxi-route</td><td>a defined path that is established for the movement of VCA from one part of a vertiport to another: • an air taxi-route: a marked taxi-route that is intended for air taxing • a ground taxi-route: a marked taxi-route centred on a taxiway that is intended for ground movement</td></tr><tr><td>VCA taxiway</td><td>a defined path on a vertiport that is intended for the ground movement of VCA from one part of a vertiport to another</td></tr></table>

![5e000f994345cc8afb8d276d4e619aca08ea8d54167832d8f7f4d5aeb96cb1a6.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5e000f994345cc8afb8d276d4e619aca08ea8d54167832d8f7f4d5aeb96cb1a6.jpg)

![ac1658b2d00162b5b73fd638e3cc6eccf7acf6683b2d7f5b39a0d1c7f50d5d7f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/ac1658b2d00162b5b73fd638e3cc6eccf7acf6683b2d7f5b39a0d1c7f50d5d7f.jpg)

# 配套专题资料（电力/运行/监管）

# FAA UAM Concept of Operations

![830a260b5cfdb808882db83cd1b351b486f20dc80817e447ba8d98ba47e1c292.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/830a260b5cfdb808882db83cd1b351b486f20dc80817e447ba8d98ba47e1c292.jpg)

Urban Air Mobility (UAM)

PAGE LEFT INTENTIONALLY BLANK

![9579dc05bf26346ab9ae31f869b83309dff4c33bdbf984958affabb11d45f1dd.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9579dc05bf26346ab9ae31f869b83309dff4c33bdbf984958affabb11d45f1dd.jpg)

U.S. Department of Transportation Federal Aviation Administration

Office of NextGen

800 Independence Ave., S.W.

Washington, DC 20591

April 26, 2023

Dear Reader:

We are pleased to share Version 2.0 of the Urban Air Mobility (UAM) Concept of Operations (ConOps) with our Federal Aviation Administration (FAA), National Aeronautics and Space Administration (NASA), and industry partners who have provided feedback to Version 1.0 of this document since its release in 2020. This ConOps documents the outcomes of the joint concept development efforts undertaken to date by the FAA NextGen Office with industry stakeholders as well as interagency coordination.

The UAM ConOps Version 2.0 is an iterative progression of work in the development of the concept that will be continued to mature through ongoing government and industry stakeholder collaboration. Future editions of the UAM ConOps will provide a broader and more comprehensive vision of our shared partnership for UAM operations based on feedback and continued collaboration surrounding this iteration of the UAM ConOps.

This document is key element in maturing the overall Advanced Air Mobility (AAM) concept aimed at developing an air transportation system that moves people and cargo between local, regional, intraregional, and urban locations not previously served or underserved by aviation using innovative aircraft, technologies, infrastructure, and operations. AAM will support a wide range of passenger, cargo, and other operations within and between urban and rural environments using new and innovative aircraft.

Sincerely,

Paul Fontaine   
Assistant Administrator for NextGen (A)   
ANG-1

PAGE LEFT INTENTIONALLY BLANK

## Executive Summary

The Federal Aviation Administration (FAA) NextGen Office released the initial Concept of Operations (ConOps) v1.0 for Urban Air Mobility (UAM) in June 2020 to describe a new, future, operational environment. UAM is a subset of Advanced Air Mobility (AAM), an initiative by the FAA, National Aeronautics and Space Administration (NASA), and industry. The AAM initiative aims to develop an air transportation system that moves people and cargo between local, regional, intraregional, and urban locations not previously served or underserved by aviation using innovative aircraft, technologies, and operations. While AAM supports a wide range of passenger, cargo, and other operations within and between urban and rural environments, UAM focuses on flight operations in and around urban areas. The UAM vision is supported by the introduction of a cooperative operating environment known as Extensible Traffic Management (xTM), which complements the traditional provision of Air Traffic Services (ATS) for future passenger or cargo-carrying operations/flights.

This concept is not a policy statement and is not a prescriptive statement of what the far term integration will be. It is a target description of the evolution of integration from the near-term Innovate 28 environment to a future of high-density urban operations. The concept focuses on a potential longer-term target supporting exploration and validation efforts. Future versions of the ConOps will reflect the outcomes of analyses, trials, concept maturation, and collaboration.

While many of the concept elements are similar across the future cooperative environments (e.g., UAM, Unmanned Aircraft Systems [UAS] Traffic Management [UTM], Upper Class E Traffic Management [ETM]), this ConOps focuses on UAM. The envisioned evolution for UAM operations includes an initial, low-tempo set of operations that leverage the current regulatory framework and rules (e.g., Visual Flight Rules [VFR], Instrument Flight Rules [IFR]) as a platform for increasing operational tempo, greater aircraft performance, and higher levels of autonomy. These are made possible by increased information sharing with operations across a range of environments, including major metropolitan areas and the surrounding suburbs. Resulting from stakeholder input sessions, the mature state operations will be achieved at scale through a crawlwalk-run approach, wherein:

1. Initial UAM operations are conducted using new aircraft types that have been certified to fly within the current regulatory and operational environment.

2. A higher frequency (i.e., tempo) of UAM operations in the future is supported through regulatory evolution and UAM Corridors that leverage collaborative technologies and techniques.

3. New operational rules and infrastructure facilitate highly automated cooperative flow management in defined Cooperative Areas (CAs), enabling remotely piloted and autonomous aircraft to safely operate at increased operational tempos.

This updated UAM ConOps v2.0 reflects the continued maturation of UAM and incorporates feedback received on v1.0, as well as research outcomes and additional input from government and industry stakeholders. Its focus is on clarifying elements from the initial version and providing additional detail in response to the feedback and input.

Language and definitions have been updated to ensure consistency across the cooperative (i.e., xTM) operating environments when applicable and includes an expanded description of Cooperative Operating Practices (COPs) (previously Community Business Rules [CBRs]). However, it does not prescribe specific solutions, detailed operational procedures, or implementation methods except as examples to support a fuller understanding of the elements associated with UAM operations.

Document Change Record
<table><tr><td rowspan=1 colspan=1>PublishedDate</td><td rowspan=1 colspan=1>DocumentVersion</td><td rowspan=1 colspan=1>SectionImpacted</td><td rowspan=1 colspan=1>Revisions of Particular Merit</td></tr><tr><td rowspan=1 colspan=1>6/26/2020</td><td rowspan=1 colspan=1>1.0</td><td rowspan=1 colspan=2>Baseline Document</td></tr><tr><td rowspan=9 colspan=2>4/26/2023        2.0</td><td rowspan=1 colspan=1>Throughout</td><td rowspan=1 colspan=1>Expanded document to provide greater detail ofselected concept elements (e.g., COPs) and relationshipof UAM within the service environments (i.e., ATS andxTM) as well as reconcile use of terms.</td></tr><tr><td rowspan=1 colspan=1>1.3</td><td rowspan=1 colspan=1>Updated and expanded service environmentdescriptions to include ATS and xTM.</td></tr><tr><td rowspan=1 colspan=1>1.4</td><td rowspan=1 colspan=1> Incorporated definitions for range of terms used acrossthe cooperative environments (e.g., UTM, UAM, AAM,xTM).</td></tr><tr><td rowspan=1 colspan=1>3.0, 3.1,3.2, 3.3</td><td rowspan=1 colspan=1>Amended to reflect updated terms and provide greaterdetail on the use of current regulatory framework tosupport initial UAM operations.</td></tr><tr><td rowspan=1 colspan=1>4.2</td><td rowspan=1 colspan=1>Addition of section focused on Cooperative OperatingPractices (COPs), which replaces Community BusinessRules (CBRs)</td></tr><tr><td rowspan=1 colspan=1>4.3.5</td><td rowspan=1 colspan=1>Updated the phrasing/language describing the federatedservice network supporting UAM operations.</td></tr><tr><td rowspan=1 colspan=1>4.4.1, 4.4.2,4.4.3, 4.4.4</td><td rowspan=1 colspan=1>Provided additional detail for elements of UAMCorridors, including potential evolution over time.</td></tr><tr><td rowspan=1 colspan=1>5.0</td><td rowspan=1 colspan=1>Updated architecture with additional details (e.g., dataexchanges specific to UAM/PSUs, depiction ofvertiports).</td></tr><tr><td rowspan=1 colspan=1>6.0</td><td rowspan=1 colspan=1>Updated scenarios to reflect current content in the bodyof the concept.</td></tr></table>

## Table of Contents

Executive Summary .................. ....... iv   
1 Introduction ...... ... 1   
1.1 Scope.... .. 1   
1.2 Background.. ..... 1   
1.2.1 Drivers for Change ..... ..... 1   
1.2.2 Aircraft Evolution... ..... 2   
1.2.3 Vertiport Considerations . .... 2   
1.3 Operating Environment Perspectives.. .... 2   
1.3.1 Overview ..... ...... 2   
1.3.2 UAM Cooperative Environment ........ ............. ....... 3   
1.3.3 Operations in the ATS Environment ... ...... 4   
1.4 Definitions . .... 4   
2 Principles and Assumptions......... ......... 5   
3 Evolution of UAM Operations ...... ...... 6   
3.1 Initial UAM Operations .. ..... 8   
3.2 Midterm Operations. .... 8   
3.3 Mature State Operations .. .... 9   
4 UAM Operational Concept....... .......... 10   
4.1 Overview....... ....... 10   
4.2 Cooperative Operating Practices (COPs) . ...... 11   
4.3 Roles and Responsibilities ... .... 12   
4.3.1 FAA ... ..... 12   
4.3.2 UAM Operator ..... ..... 13   
4.3.3 Pilot in Command (PIC).. .... 13   
4.3.4 Provider of Services for UAM (PSU) . ... 13   
4.3.5 Federated Service Network . ..... 15   
4.3.6 Supplemental Data Service Provider (SDSP) ... ............. ........ 15   
4.3.7 UAM Vertiport ......   
4.3.8 UAS Service Supplier (USS) ... ....... 15   
4.3.9 Other NAS Airspace Users... .... 16   
4.3.10 Public Interest Stakeholders .... ..... 16   
4.4 UAM Corridors.. .. 16   
4.4.1 UAM Corridor Entry/Exit Points (CEPs). .. 18   
4.4.2 Conflict Management and Separation .... ..... 19   
4.4.3 Demand-Capacity Balancing (DCB).. ... 19   
4.4.4 UAM Corridor Evolution . .. 20   
4.5 Weather and Obstacles Within the UAM Environment . .. 22   
4.6 Constraint Information and Advisories.. ... 22   
5 Notional Architecture....... ..... 23   
5.1 Supporting Services ... ..... 24   
6 UAM Scenarios .... ... 24   
6.1 Nominal UAM Operation Completed Within a UAM Corridor.. .. 25   
6.1.1 Planning Phase .. ... 25   
6.1.2 In-Flight Phases ... .... 25   
6.1.3 Post-Operations Phase.... .... 26   
6.2 Nominal UAM Operation Across Service Environments.... .... 26   
6.2.1 Planning Phase ... ... 26   
6.2.2 In-Flight Phases .. ... 27   
6.2.3 Post-Operations Phase. ... 28   
7 UAM Evolution ...... ..... 28   
Appendix A References...... ..... 29   
Appendix B Acronyms... ... 30   
Appendix C Glossary ........... .... 32

## List of Figures

Figure 1: Notional Overview of Future Complementary Service Environments . . 3   
Figure 2: Evolution of the UAM Operational Environment. .. 7   
Figure 3: Notional Multiple UAM Corridors... ... 18   
Figure 4: Early UAM Corridor Concept.. .. 20   
Figure 5: Use of a Vertical Common Passing Zone ... 21   
Figure 6: Use of Lateral Passing Zones .. ... 21   
Figure 7: UAM Corridor with Multiple Tracks . .. 22   
Figure 8: Notional UAM Architecture.. .. 24

## List of Tables

Table 1: Acronyms... .. 30   
Table 2: Glossary .. . 32

## 1 Introduction

## 1.1 Scope

Urban Air Mobility (UAM) enables highly automated, cooperative, passenger or cargo-carrying air transportation services in and around urban areas. UAM is a subset of the Advanced Air Mobility (AAM) concept under development by the Federal Aviation Administration (FAA), National Aeronautics and Space Administration (NASA), and industry. As a subset of AAM, UAM focuses on operations moving people and cargo in metropolitan and urban areas. This Concept of Operations (ConOps) provides an evolving vision that will help facilitate further research on how to best assist UAM operations in the National Airspace System (NAS) if demand and volume exceed current capabilities.

The goal of this ConOps is to provide a common frame of reference to support the FAA, NASA, industry, and other stakeholder discussions and decision-making with a shared understanding of the challenges, technologies, and their potential, as well as examples of areas of applicability to the NAS. No solutions, specific implementation methods, or detailed operational procedures are described in this document except for example purposes (i.e., operational scenarios). This ConOps will be further matured and updated as the concept undergoes validation, stakeholder engagement continues, and additional operational scenarios are developed.

As the follow-on to the UAM ConOps v1.0, this document reflects the outcome of additional stakeholder engagement, exploration, and validation activities. It represents the continued maturation of the vision for UAM operations, airspace considerations, and UAM Cooperative Operating Practices (COPs). The ConOps v2.0 identifies the need for regulatory changes to support operations and collaborative environments with increasing density and complexity.

Current industry projections describe initial UAM operations incorporating a Pilot in Command (PIC) onboard the UAM aircraft with potential evolution to Remote PIC (RPIC). Consistent with the ConOps v1.0 and industry expectations, this document describes operations with an onboard PIC operating within the cooperative environment.

## 1.2 Background

Transportation is constantly evolving. Each step forward yields new opportunities that fundamentally change the relationship that humankind has with distance and travel. While it may not significantly reduce surface traffic volume, UAM will provide an alternative mode of transportation that should reduce traffic congestion during peak times.

## 1.2.1 Drivers for Change

For the UAM concept to mature to operational viability, it is important to understand stakeholder business models and operational needs, as well as their impact, for incorporation into the NAS. The FAA has collaborated with NASA and participated in a series of additional industry stakeholder engagements to identify examples of desired operations and environments for UAM aircraft.

The volume of UAM operations may increase substantially. The degree to which some, or all, of these UAM operations will require current Air Traffic Services (ATS) is undefined. To the degree that these operations require current ATS, the increasing number of UAM operations may soon challenge the current capabilities of the ATS workforce resources. Solutions that extend beyond the current paradigm for crewed aircraft operations to those that promote enhanced shared situational awareness and collaboration among operators are needed. As the FAA continues to mature the UAM concept, additional support systems for UAM operators may be introduced.

To the degree that these operations require current ATS, the increasing number of UAM operations could create new challenges for ATS workforce resources. Several industry leaders and stakeholders have invested heavily in this new concept and technology with the goal of eventually being able to provide the public with personal transportation or cargo services. Personal transportation services may be scheduled, on demand, or part of intermodal transportation links within major urban areas. Greater public acceptance of aircraft integrity and automation in the ride sharing economic model will also help enable increased UAM operations.

## 1.2.2 Aircraft Evolution

The industry vision involves incorporating new aircraft design and system technologies. While some of the new designs may resemble traditional winged aircraft, some are anticipated to include powered lift and Vertical Takeoff and Landing (VTOL) capabilities that facilitate operations between desired locations (e.g., metropolitan commutes). Major aircraft innovations, mainly with the advancement of Distributed Electric Propulsion (DEP) and development of Electric VTOLs (eVTOLs), may allow for these operations to be utilized more frequently and in more locations than are currently performed by conventional aircraft.

## 1.2.3 Vertiport Considerations

State and local governments are being encouraged to actively plan for UAM infrastructure to ensure transportation equity, market choice, and accommodation of demand for their communities. The vertiports and vertistops should be sited to ensure proper room for growth based on FAA evaluated forecasts and be properly linked to surface transportation (when possible), especially if the facility primarily supports cargo operations. Local governments should also have zoning protections in place to protect airspace in and around vertiports and vertistops.

Metropolitan planning organizations, including state and local governments, may incorporate UAM infrastructure planning into larger transportation and utility planning efforts to ensure seamless coverage and capacity. Community engagement and strategic connectivity to larger transportation planning efforts is key to ensuring UAM provides maximum benefits.

## 1.3 Operating Environment Perspectives

## 1.3.1 Overview

NAS operating environments include the airspaces, types of operations, regulations, and procedures necessary to support an operation. Currently, the range of NAS services provided to airspace users are characterized at the highest level under the category of ATS. These include separation (via Air Traffic Control [ATC]), Traffic Flow Management (TFM), advisories, and infrastructure (i.e., Communication, Navigation, and Surveillance [CNS]). Evolving concepts describe the introduction of highly automated, cooperative environments such as Unmanned Aircraft Systems (UAS) Traffic Management (UTM), AAM/UAM, and Upper Class E Traffic Management (ETM) to meet future NAS needs and challenges. These concepts of operations rely on sharing intent information across airspace users. This is governed by the current, evolving regulatory framework as needed to support new types of operations in defined Cooperative Areas (CAs) within which they are conducted.

## 1.3.2 UAM Cooperative Environment

Recent advances in technology have enabled industry development of new and innovative aircraft types, offering lower operating costs and highly automated functionality that facilitates the introduction of new types of operations. At the same time, advances in real-time information sharing and the distribution of roles and functions over federated service networks are maturing daily. In response to these challenges and opportunities, a highly automated, cooperative environment (with defined CAs) relying on a federated service network has been envisioned and described through multiple operational concepts as an additional aspect of the future service environments and part of the NAS. The term Extensible Traffic Management (xTM) is used to refer to these cooperative service environments in general and is comprised of UTM, AAM/UAM, and ETM. UAM operations, as a subset of AAM, may sometimes be conducted in CAs generally described as UAM Corridors. The evolution of the regulatory framework will provide the needed guidance to allow application of the innovative concepts, technologies, and techniques to support the emerging aircraft types and envisioned operations. Figure 1 provides a depiction of the AAM/UAM environment (outlined in red) relative to the current service delivery environment, as well as the other future cooperative environments.

As part of the future NAS, the complementary service delivery environments (i.e., ATS and xTM) will be evaluated as potential options to assist with scalability to meet future demand challenges and the flexibility to seize opportunities presented by the rapid evolution across the technology horizon (e.g., cloud computing, communications, information management).

![46b479d47ea514b2168df35aa0f7b599a07bd9e54509dd65ceb3d4b8aec00cdb.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/46b479d47ea514b2168df35aa0f7b599a07bd9e54509dd65ceb3d4b8aec00cdb.jpg)  
Figure 1: Notional Overview of Future Complementary Service Environments

## 1.3.3 Operations in the ATS Environment

All aircraft are required to comply with the regulatory requirements of the airspace within which they are conducting operations. A UAM operation is one executed by a UAM aircraft conducted within an airspace volume defined for UAM cooperatively managed operations. When conducting operations in the ATS environment, a UAM aircraft will comply with the ATS requirements of the applicable airspace class.

UAM aircraft will need to comply with applicable ATS regulations regarding VFR and IFR while operating in either Visual Meteorological Conditions (VMC) or Instrument Meteorological Conditions (IMC), like any current NAS operation. Capable aircraft (and operators) may choose to utilize ATS operating outside of a CA or cooperative services if operating in a CA based on whichever is more operationally advantageous to the airspace user. Consistent with today’s operations, this choice is subject to the environment and conditions for the flight.

## 1.4 Definitions

Automated Flight Rules (AFRs) – Refers to rules, applied within UAM Corridors, which reflect the evolution of the current regulatory regime (e.g., VFR/IFR) and take into account advancing technologies and procedures (e.g., Vehicle-to-Vehicle [V2V] and data exchanges). Under defined conditions, the systems/automation may be allocated the role of the “predetermined separator” (see paragraphs 2.7.18–2.7.22 in [1]).

Cooperative Area – An airspace volume (e.g., UAM Corridor) within which cooperatively managed operations can occur. ATC ensures separation of non-participating aircraft from the cooperative operations and/or CA.

Cooperative Operating Practices (COPs) – Industry-defined, FAA-approved practices that address how operators cooperatively manage their operations within the CA (i.e., UAM Corridor), including conflict management, equity of airspace usage, and Demand-Capacity Balancing (DCB).

Cooperative Operation – A term used to describe an operation making use of cooperative services (e.g., separation, flow management) and is sharing/exchanging Operational Intent and other information in compliance with applicable regulations and COPs within a CA.

Federated Service Network – A group of service providers sharing information within a federated network to support operating in a common, agreed manner consistent with the approved COPs.

Fully Integrated Information Environment – Information environment and key attributes necessary to effectively deliver services and facilitate information exchange between stakeholders.

Service Environment(s) – Refers collectively to the distinct regulatory, procedural, and supporting automation mechanisms through which services (e.g., conflict management, flow management) are provided. In the future, the NAS is envisioned to include the current (i.e., traditional) ATS environment as well as incorporate a complementary, cooperative xTM services environment.

UAM Aircraft – An aircraft that chooses to participate in UAM operations.

UAM Corridor – A specific type of CA, as an airspace volume within which cooperatively managed operations can occur. ATC ensures separation of non-participating aircraft from the cooperative operations and/or CA. It is comprised of an airspace volume defining a threedimensional route, possibly divided into multiple segments, with associated performance requirements.

UAM Operation – A specific type of cooperative operation that occurs within a UAM Corridor and is conducted in compliance with UAM specific rules, procedures, performance requirements, and COPs.

UAM Operator – The person or entity responsible for the overall management and execution of one or more UAM operations. The operator plans operations, shares flight information (e.g., planning, live flight), and ensures infrastructure, equipment, and services are in place to support safe execution of flight. Throughout this document, “UAM operator” is often used to describe the roles and responsibilities of the UAM Code of Federal Regulations (CFR) Title 14, Part 135 carrier, the RPIC/PIC, or conflict management automation to avoid allocating prematurely and allow for evolution of the role.

Vertiports – A collective term for the diverse system of public and private vertiports and vertistops.

Vertiport – An area of land or structure used or intended to be used for electric, hydrogen, and hybrid VTOL landings and takeoffs. A vertiport can include associated buildings and facilities.

Vertistop – A vertistop is a term generally used to describe a minimally developed vertiport for boarding and discharging passengers and cargo (i.e., no fueling, defueling, maintenance, repairs, or storage of aircraft, etc.).

## 2 Principles and Assumptions

The following principles and assumptions guide the development of the UAM operating environment and mature the UAM concept.

• The FAA retains regulatory authority over NAS airspace and operations.

o UAM aircraft operate within a regulatory, operational, and technical environment as part of the NAS.

o Any evolution of the regulatory environment will always maintain safety of the NAS.

• The FAA reserves the right to increase aircraft operational performance requirements to optimize the capacity/utilization of the airspace.

• The FAA has on-demand access to information regarding UAM operations.

• Airspace management will be static where necessary and flexible when possible.

• UAM operators:

o Are responsible for the coordination, execution, and management of their operations.

o Conduct operations in compliance with the applicable regulatory framework for the operation, the airspace within which the operation is conducted, and the applicable COPs.

O Maintain conformance to shared intent and, via Providers of Services for UAM (PSUs), are made aware of the intent of other relevant operations.

o Cannot optimize their own operations at the expense of sub-optimizing the environment as a whole.

Cooperative traffic management is conducted in compliance with a set of COPs, which would need to be collaboratively developed by relevant stakeholders and approved by the government.

o DCB intervention may be required as the number of UAM operations increases.

o As the operational tempo increases the need for new ATC tactical deconfliction techniques, including the formulation of new separation standards that would rely on enhanced aircraft performance and air traffic management system fidelity may be utilized.

o The architecture (i.e., technology) for UAM services needs to be flexible and scalable. Operators or third-party service suppliers share information using common standards and messaging protocols to ensure interoperability.

• PSUs may be utilized by operators to receive and exchange information during UAM operations.

## 3 Evolution of UAM Operations

The evolution of UAM operations is characterized by the following key indicators.

1. Operational Tempo: Representation of the density, frequency, and complexity of UAM operations. Tempo evolves from a small number of low-complexity operations to a highdensity, high frequency of complex operations.

2. UAM Structure (Airspace and Procedural): The level of complexity of infrastructure and services that support the UAM environment.

3. UAM-Driven Regulatory Changes: Existing regulations may need to evolve to address the needs for UAM operations’ structure and performance.

4. UAM COPs: COPs implement the updated regulations to establish the expectations and interactions. See Section 4.2 for additional COP details.

5. Aircraft Automation Level: The level of “PIC” engagement with the UAM aircraft enabling systems. The following categories describe the evolution of aircraft automation:

Human-Within-the-Loop (HWTL)

o Human is always in direct control of the automation (i.e., systems)

Human-on-the-Loop (HOTL)

o Human has supervisory control of the automation (i.e., systems)

o Human actively monitors the systems and can take full control when required or desired

Human-Over-the-Loop (HOVTL)

o Human is informed, or engaged, by the automation (i.e., systems) to take action

o Human passively monitors the systems and is informed by automation if, and what, action is required

o Human is engaged by the automation either for exceptions that are not reconcilable or as part of rule set escalation

6. Location of the PIC: The physical location of the PIC. UAM operations may evolve from a PIC onboard the UAM aircraft to RPICs/remote operators via the advent of additional aircraft automation technologies.

Figure 2 describes the evolution of UAM operations and its relationship with increasing level of operational tempo and the airspace structure and procedures.

![8d0b7f2cc39d5583af4bdcb5ba8b47a6f6842e1ec651ed129d314de85342e366.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/8d0b7f2cc39d5583af4bdcb5ba8b47a6f6842e1ec651ed129d314de85342e366.jpg)  
Figure 2: Evolution of the UAM Operational Environment

UAM operational evolutionary stages are described in the following subsections:

Initial UAM operations

• Midterm operations

• Mature state operations

## 3.1 Initial UAM Operations

Initial UAM operations are conducted by UAM aircraft leveraging current ATS rules and regulations (e.g., VFR, IFR). Key indicators of initial UAM operations are listed below.

Operational Tempo: Low.

UAM Structure (Airspace and Procedural): No UAM unique structures or procedures exist. Operations will utilize existing ATS and routes but may create new routes as necessary.

UAM-Driven Regulatory Changes: Initial UAM operations are conducted leveraging current rules, regulations, and local agreements.

• UAM COPs: There are no COPs, but operational needs may be addressed in agreements such as Letters of Agreement (LOAs).

• Aircraft Automation Level: Consistent with current, crewed fixed-wing and helicopter technologies (e.g., autopilots, auto-land).

• Location of the PIC: Onboard.

For UAM aircraft that are capable, current operations are supported by existing rules, procedures, and designated routes. As additional operations outside of the current operational paradigms are initiated, LOAs, routes, and other procedural changes may need to be introduced to accommodate the additional demand and location of operations within the regulatory framework of the current ATS system. Since industry anticipates increasing operations to scale cost effectively and meet increased demand for services, the demand for UAM operations may eventually reach the limits of current regulations and ATS services.

## 3.2 Midterm Operations

With increased tempo, UAM operations will evolve through changes to the governing regulations augmented by COPs, UAM infrastructure, and automation. The evolution to a collaborative, information-rich, data-sharing environment may require new technologies and capabilities. UAM operators and other stakeholders will share information with the FAA, having on-demand access to identified operational information.

Midterm operations are supported by an environment that meets the needs of increased operational tempo. Key indicators of midterm UAM operations are listed below.

Operational Tempo: The operational tempo remains low; however, it may have increased to a point that necessitates changes in the existing regulatory framework and procedures.

UAM Structure (Airspace and Procedural): UAM aircraft are flying within UAM Corridors. UAM operations are enabled through confirmed UAM Operational Intent— operation-specific information including, but not limited to, UAM operation identification, the intended UAM Corridor(s), aerodromes and vertiports, and key operational event times (e.g., departure, arrival) of the UAM operation. Operations are considered UAM participants during the period of operation that exists within the UAM Corridor cooperative environment.

ATC ensures separation of non-participating aircraft from cooperative operations and/or CAs.   
Deconfliction may be allocated to the UAM operator and/or PIC akin to visual separation.

UAM-Driven Regulatory Changes: Changes to ATS regulations and new UAM regulations that enable operations within UAM Corridors.

UAM COPs: COPs are defined by industry to meet industry standards or FAA guidelines when specified. COPs will require FAA approval.

• Aircraft Automation Level: PICs may control the aircraft with emerging capabilities (e.g., simplified vehicle operation).

• Location of the PIC: Primarily onboard aircraft but complemented by the introduction of RPIC operations (with one RPIC per operation).

The number and complexity of operations, along with aircraft capabilities and equipage, may increase beyond that effectively supported by leveraging current rules (e.g., VFR, IFR). To support such an increase, a UAM cooperative environment may need to be developed and implemented with new or modified procedures, an updated regulatory framework, and COPs. The UAM cooperative environment (i.e., UAM Corridor) is a performance-based airspace structure with defined parameters that are achievable by the participants. UAM Corridors would be known to airspace users and governed by a set of rules which prescribe access and operations. Where supporting infrastructure and support services meet participation requirements, UAM operations may be conducted. Operators whose aircraft meet performance and participation requirements may conduct operations within the UAM Corridor.

Initially, the number of UAM Corridors may be low or limited in use, but over time, additional UAM Corridors may be introduced as they may be utilized in airspace areas where traffic volume requires their establishment in the interest of safety and efficiency. The UAM Corridors may transit any applicable airspace classes.

Operations within UAM Corridors may be supported by COPs collaboratively developed by the stakeholder community, based on industry standards and/or FAA guidelines, and approved by the FAA, as appropriate, to ensure that the agency’s regulatory authority is maintained (e.g., NAS safety, equitable access, security). The collaborative development of COPs would allow for stakeholders to agree on norms of interactions, which may reduce the need for ATC tactical control of individual flights and management of access. The collaboratively developed, transparent, standard COPs augment the envisioned regulatory foundation for UAM operations.

## 3.3 Mature State Operations

As the UAM operational tempo increases, UAM operations may further evolve to support operational demand. Key indicators of mature state UAM operations are listed below.

Operational Tempo: The operational tempo increases significantly. Higher operational tempo needs drive the increased maturity for the other indicators.

UAM Structure (Airspace and Procedural): UAM operations continue to occur within UAM Corridors. The UAM Corridors may form a network to optimize paths to support an increasing number of vertiports; the internal structure of the UAM Corridors is expected to increase in complexity, and the necessary performance parameters for UAM participation may increase. ATC ensures separation of non-participating aircraft from cooperative operations/CAs. Deconfliction may be allocated to the UAM operator, PIC, or operator’s automation.

• UAM-Driven Regulatory Changes: Extensive UAM-driven regulations will be necessary to enable cooperative operations within UAM Corridors.

UAM COPs: The complexity of COPs and FAA involvement in establishing guidelines and approving COPs may evolve to match the specific topic addressed.

• Aircraft Automation Level: Automation improvements may lead to HOVTL capabilities.

• Location of the PIC: Remote piloting is more widely available and as frequent as PIC operations.

Additional increases in the tempo of midterm operations could require advances to the UAM environment and aircraft. To overcome the constraints, UAM operations may evolve to UAM mature state operations through advances to data sharing, DCB, UAM structure, and aircraft automation. Mature state operations may also include additional COPs accompanied by UAMdriven regulatory changes.

## 4 UAM Operational Concept

This section provides an overview of the UAM operational concept and COPs, followed by key definitions and descriptions of roles and responsibilities, UAM Corridor characteristics, weather and other obstacles within the UAM environment, and constraint information and advisories.

## 4.1 Overview

A UAM operator performing a UAM operation is cooperatively sharing information and engaging cooperative services to assure the safe and efficient conduct of the flight within a UAM Corridor. The UAM Corridor structure, UAM procedures, information sharing, and UAM performance criteria enable increasing operational tempo and minimize impact to ATS. UAM operations are supported by PSUs that comprise a federated service network to enhance the capabilities of individual UAM operators/PICs in all phases of operations through exchange, analysis, and mediation of information among all relevant actors (e.g., UAM operators/PICs, PSUs, the FAA, and public interest stakeholders).

Any aircraft operating within a UAM Corridor must meet the performance and participation requirements of the UAM environment. Within UAM Corridors, deconfliction is allocated by ATC to UAM operators and/or PIC. The UAM community will collaboratively develop and establish COPs as standards for operations. The FAA may contribute to COP guidelines but will approve COPs based on the specific focus, topic, or area addressed by the COP. UAM Corridor design, performance, and participation requirements, as well as UAM COPs, may be designed to reduce ATC involvement with UAM off-nominal events by implementing standardized off-nominal protocols. UAM aircraft operating outside UAM Corridors must follow the operational rules and procedures applicable to the corresponding airspace.

The concept represents an early step in the envisioned evolution of the regulatory framework, development of operating rules and performance requirements commensurate with demands of the operation, and data exchange with information architecture to support UAM operator and FAA responsibilities. UAM leverages a common, shared, technical environment, where the operators are responsible for coordination, execution, and management of operations consistent with the regulatory framework and applicable COPs. This networked information exchange is the cornerstone for stakeholders to plan, manage, execute, and oversee UAM operations. Additional stakeholders can access UAM shared operational information on demand.

## 4.2 Cooperative Operating Practices (COPs)

Foundational to the success of the envisioned, federated, highly automated, cooperative environment is the establishment of common business rules across relevant stakeholders, referred to as COPs. Development, adoption, and implementation of COPs will require collaboration across multiple stakeholders—including operators, industry, and the FAA as the regulator—to identify and resolve a broad range of questions and challenges. Examples of these questions include “what rules are needed?”, “how are they expressed?”, and “how will they be managed?”

COPs are characterized as industry-defined, FAA-approved practices that address how operators cooperatively manage their operations within the cooperative UAM environment, including conflict management, equity of airspace usage, and DCB.

They are consistent with and augment updates to the regulatory framework. 1 The development timeframe will be driven by the pace at which operators desire to execute cooperative UAM operations distinct from those conducted under the current regulatory framework (e.g., VFR, IFR). As the tempo and complexity of UAM operations increases, it is anticipated that the complexity and range of topics covered by COPs will also increase. The relationship between industry and government (e.g., FAA, Department of Transportation [DOT]) differs based on the focus of the specific COP. In some instances, the rules or topic area of an individual COP may determine the level of engagement necessary with the regulatory authority. The level of engagement also has implications for the level of involvement that the authority will undertake as part of the applicable coordination for the specific COP. The range of engagement by the regulator may span from minimal to high levels. At higher levels, significant documentation, and testing, as well as formal acceptance, authorization, or qualification, may be necessary prior to operational use by industry.

Another aspect of the relationship between government and industry before a specific COP may be used operationally is “equity interest.” This refers to how closely the topic/area covered by the specific COP is related to government responsibilities (i.e., mission) or policies. Some COPs, such as those focused on aviation safety, fall directly under the FAA’s regulatory mission. Other COPs, such as avoiding unnecessary anti-competitive technical specifications for participation in the federated service network, may be subject to policies that fall under the purview of regulatory agencies beyond the FAA.

## 4.3 Roles and Responsibilities

This section defines the roles and responsibilities for actors associated with UAM operations.

## 4.3.1 FAA

The FAA performs regulatory, ATC, and NAS data exchange roles for UAM, as detailed in the following subsections.

## 4.3.1.1 Regulation

The FAA is the federal authority over aircraft operations in all airspace and the regulatory and oversight authority for civil operations in the NAS. The FAA maintains an operating environment that ensures airspace users have access to the resources needed to meet specific operational objectives and that shared use of the airspace can be achieved safely and equitably. The FAA develops or modifies regulations to support UAM operations. The FAA will approve COPs to ensure that the FAA authority is maintained (e.g., NAS safety, equal access to airspace, security). The FAA will define, maintain, and make publicly available UAM Corridor definitions (e.g., routes and altitudes) and manage the performance requirements of UAM Corridors.

## 4.3.1.2 ATC

The primary purpose of ATC is to maintain safe movement of aircraft operating within the NAS. For high-density UAM operations, this may be accomplished through ATM modernization. ATC will ensure the separation of non-participating aircraft from the cooperative operation and/or CAs. As appropriate, ATC may issue traffic advisories regarding known UAM operations (e.g., active UAM Corridors) to aircraft receiving ATC services. ATC may request information as needed from participating actors and may receive automated notifications in accordance with applicable requirements.

The ATC responsibilities that enable UAM operations are to:

1. Set UAM Corridor availability (e.g., open or closed) based on operational design (e.g., time of day, flow direction of a nearby airport).

2. As appropriate, provide traffic advisories regarding known UAM operations (e.g., active UAM Corridors) to aircraft receiving ATC services.

3. Respond to UAM off-nominal operations as needed.

4. When tactical separation assurance is required, provide current or newly developed services appropriate to the airspace in which the UAM aircraft is operating.

To fulfill their responsibilities, ATC may review any pertinent information from UAM operations.

## 4.3.1.3 NAS Data Exchange

FAA NAS data sources are available to UAM operations via FAA-industry exchange protocols.   
This allows for authorized data flow between the UAM community and FAA operational systems.

This interface between the FAA and UAM stakeholders is a gateway such that external entities do not have direct access to FAA systems and data. FAA data sources available via the FAA-industry data exchange include, but are not limited to, flight data, restrictions, charted routes, and active Special Activity Airspaces (SAAs).

## 4.3.2 UAM Operator

UAM operators may conduct operations as scheduled services or on-demand services via a request from an individual customer or intermodal operator. UAM operators are responsible for regulatory compliance and all aspects of UAM operation execution. Use of the term “UAM operator” in this document indicates airspace users electing to conduct operations via cooperative management within the UAM environment.

The UAM operator obtains current conditions from PSU and Supplemental Data Service Provider (SDSP) services (e.g., environment, situational awareness, strategic operational demand, vertiport availability, supplemental data) to determine the desired UAM Operational Intent information. This may include location of flight (e.g., vertiport locations), route (e.g., specific UAM Corridors), UAM Corridor entry or exit point, and estimated flight time.

UAM operators must have a confirmed UAM Operational Intent to operate in UAM Corridors.   
UAM Operational Intent data serves the following primary functions.

1. Informs other UAM operators of nearby operations within the UAM Corridor to promote safety and shared awareness

2. Enables strategic deconfliction

3. Enables identification and distribution of known airspace constraints and restrictions for the intended area of operation

4. Enables distribution of spatially and temporally relevant advisories, weather, and supplemental data

5. Supports cooperative separation management services (e.g., conformance monitoring, advisory services)

The UAM operator also plans for off-nominal events. This includes an understanding of alternative landing sites and the airspace classes that border the UAM Corridor(s) for the operation. Upon completion of the operation, the UAM operator notifies the PSU.

## 4.3.3 Pilot in Command (PIC)

The PIC is the person aboard the UAM aircraft who is ultimately responsible for the operation and safety during flight. This ConOps assumes a pilot onboard the aircraft; however, operations described do not preclude a remote pilot or automated operations.

## 4.3.4 Provider of Services for UAM (PSU)

A PSU is an entity that supports UAM operators with meeting UAM operational requirements that enable safe, efficient, and secure use of the airspace. A PSU is the primary service and data provider for UAM stakeholders and the interface between the UAM ecosystem and the FAA. A PSU can be a separate entity from the UAM operator, or an operator can act as its own PSU. When confirming the UAM Operational Intent, a PSU may act on behalf of an operator who has subscribed to its offered services within the updated regulatory framework established by the FAA for instances when an operator does not act as its own PSU.

## A PSU:

1. Provides a communication bridge between federated UAM actors, from PSU to PSU via the network, to support its subscribing UAM operator’s ability to meet the regulatory and operational requirements for UAM operations.

2. Provides its UAM operators with information gathered from the network about planned UAM operations in a UAM Corridor so that UAM operators can ascertain the ability to conduct safe and efficient missions.

3. Analyzes and confirms that a submitted UAM Operational Intent is complete, consistent with current advisories and restrictions, and strategically deconflicted considering previously confirmed UAM Operational Intents, COPs, UAM Corridor capacity, airspace restrictions, vertiport resource availability, and adverse environmental conditions.

4. Provides the confirmed UAM Operational Intent to the federated service network.

5. Distributes notifications (e.g., constraints, restrictions) for the intended area of operation.

6. Distributes FAA operational data and advisories, weather, and supplemental data.

7. Supports cooperative separation management services (e.g., conformance monitoring, advisory services).

a. Assists with coordinating UAM Corridor use status; UAM Corridor use status (e.g., occupied, unoccupied) is an indication that UAM operations are being conducted or not.

8. Archives operational data in historical databases for analytics, regulatory, and UAM operator accountability purposes.

9. Negotiates airport access through the airport’s sponsor.

These key functions allow a PSU to support cooperative management for UAM operations without direct FAA involvement on a per flight basis.

PSU services support operations planning, UAM Operational Intent sharing, deconfliction, airspace management functions, and off-nominal operations that UAM operators may encounter. PSUs may provide value-added services to subscribers that optimize operations or provide SDSP services in support of UAM operations. PSUs exchange information with other PSUs via the federated service network to enable UAM services (e.g., exchange of UAM Operational Intent information, notification of UAM Corridor status, information queries). PSUs also support local municipalities and communities as needed to gather, incorporate, and maintain information that may be accessed by UAM operators.

## 4.3.5 Federated Service Network

The federated service network is the collection of connected PSUs that share subscriber information, FAA data, supplemental data, and data from other entities (e.g., PSUs, FAA, public interest stakeholders) to provide a fully integrated information environment to support UAM operations. Since multiple PSUs can provide services in the same geographical area, the federated service network facilitates the availability of data to the FAA and other entities as required to ensure safe operation of the NAS and any other information sharing functions including security and identification.

## 4.3.6 Supplemental Data Service Provider (SDSP)

UAM operators and PSUs use supplemental data services to access supporting data including, but not limited to, terrain, obstacle, and specialized weather. PSUs are also able to serve as SDSPs for subscribed UAM operators. SDSPs may be accessed via the federated service network or directly by UAM operators.

## 4.3.7 UAM Vertiport

Vertiports, used as a collective term, are expected to be a diverse system of public and private vertiports and vertistops. These facilities are categorized to identify the variety of aircraft they can support based on facility design and operations. Vertiports and vertistops support passenger and cargo operations for aircraft operating in VFR, IFR, and AFR.

UAM operators are expected to utilize whichever vertiport configuration meets their operational needs.

A vertiport is a designated area that meets the capability requirements to support UAM departure and arrival operations. The UAM vertiport provides current and future resource availability information for UAM operations (e.g., open/closed, pad availability) to support UAM operator planning and PSU strategic deconfliction. UAM vertiport information is accessible by the operator via the federated service network and supplemental vertiport information may be available via the SDSP. The vertiport information is used by UAM operators and PSUs for UAM operation planning including strategic deconfliction and DCB; however, the vertiports do not provide strategic deconfliction or DCB services.

## 4.3.8 UAS Service Supplier (USS)

UAS Service Suppliers (USSs) are entities that support UAS operations under the UTM system (see the UTM ConOps v2.0 [2] for more details). Potential scenarios may exist where USSs and PSUs need to share information to ensure cooperative separation during UAM landing and takeoff phases of flight within UTM environments (i.e., under 400 feet).

From a UAM operational perspective, USSs may interact with PSUs by:

1. Enabling UTM operations to use federated service network services to cross a UAM Corridor.

2. Supporting UAM off-nominal operations as needed (e.g., UAM operations executing emergency landings impacting UTM operation areas).

3. Supporting UTM off-nominal operations as needed (e.g., UTM operation deviating from filed Operational Intent near a UAM vertiport).

## 4.3.9 Other NAS Airspace Users

Other NAS airspace users are any non-UAM aircraft operation within the NAS. These users would have the responsibility to know about and meet the relevant performance and participation requirements to operate in open UAM Corridors or avoid active UAM Corridors. UAM Corridor definitions and availability will be publicly available for these users to access.

## 4.3.10 Public Interest Stakeholders

Public interest stakeholders are entities declared by governing processes (e.g., COPs) to be able to access UAM operational information and notifications. This access may support activities including, but not limited to, public right to know, government regulatory, government assured safety and security, and public safety. Examples of public interest stakeholders are local law enforcement and United States federal agencies.

## 4.4 UAM Corridors

As described earlier, initial UAM operations are expected to make use of the flexibility in the current regulatory framework (e.g., VFR, IFR) to meet their operational and mission needs. Over time, the number of UAM operations are expected to increase, the specific areas/locations where operators desire to conduct the operations may expand, and aircraft capabilities (e.g., equipage, performance) could advance. Corridors may offer the opportunity to respond to what could be new levels and types of service demands while taking advantage of the aircraft’s capabilities without adversely impacting current service levels.

The concept of UAM Corridors envisions safe and efficient UAM operations that may not require traditional ATC services in certain situations, are available to any aircraft appropriately equipped to meet the performance requirements, and would be created/implemented when operationally advantageous. The UAM Corridors could help support the increasing operational tempo through increased capabilities (e.g., aircraft performance), UAM Corridor structure, and UAM procedures. At increased UAM traffic levels, UAM Corridors could be a mechanism for distinguishing and keeping separate the different regulatory frameworks—those applicable to UAM operations versus those operating under the current (e.g., IFR, VFR) or UTM regulations.

UAM Corridors would be designed consistent with applicable environmental considerations and may be implemented in areas where it is operationally advantageous. The UAM Corridors may transit all airspace classes. It is anticipated that UAM Corridors may exist simultaneously at locations and in airspace classes with constructs (e.g., VFR flyways/corridors, IFR) leveraged for initial UAM operations.

Operations within UAM Corridors may have operational performance and participation (e.g., UAM Operational Intent sharing, deconfliction within the UAM Corridor) requirements. The performance and participation requirements for a UAM Corridor may vary between UAM Corridors. In addition, performance requirements and UAM Corridor definition (e.g., volume, location) support accommodations for most UAM off-nominal operations where the UAM aircraft can complete the operation safely. Any operator meeting the UAM Corridor performance and participation requirements may operate within or crossing the UAM Corridor. The crossing of a UAM Corridor by an aircraft/operator not participating in the cooperative environment (e.g., general aviation) remains an area of exploration as the UAM Corridor concept, specific features, uses, and requirements mature. As UAM Corridor geometry is better understood, the foundational elements of UAM Corridor crossings may be analyzed by stakeholders.

UAM Corridor definitions are available to stakeholders for planning and operational use. ATC will be involved in the implementation and execution of UAM Corridors for the airspace for which ATC is responsible. Other NAS users will be aware of UAM Corridors through airspace familiarization associated with flight planning or ATC flight plan approval or advisories. UAM Corridor design considerations should include:

1. Minimal impact to existing ATS and UTM operations while maintaining equity for all operators.

2. Public interest stakeholder needs (e.g., local environmental and noise, safety, security).

3. Stakeholder utility (e.g., customer need).

UAM Corridor availability (e.g., open, closed) would be in accordance with ATC operational design (e.g., nearby airport configurations/change). UAM Corridor availability may be communicated through the federated service network to PSUs and UAM operators. In addition to UAM Corridor availability established by ATC, PSUs determine UAM Corridor status that identifies if one or more UAM operations are occurring somewhere within the UAM Corridor. UAM Corridor usage information may be used by the FAA or other stakeholders for situational awareness.

Initially, the UAM Corridors may support point-to-point UAM operations. As UAM operations evolve, UAM Corridors may be segmented and connected to form more complex and efficient networks of available routing between points (e.g., vertiports). Figure 3 shows a small number of point-to-point UAM Corridors.

![5411c6131d5533e51bad2f97e7338dc65ede154d5e37016098c1427746b10187.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5411c6131d5533e51bad2f97e7338dc65ede154d5e37016098c1427746b10187.jpg)  
Figure 3: Notional Multiple UAM Corridors

## 4.4.1 UAM Corridor Entry/Exit Points (CEPs)

Some UAM operations may be conducted wholly within the cooperative environment. However, most operations are anticipated to transit both service environments (i.e., ATS and xTM [UAM]). Corridor Entry/Exit Points (CEPs) refer to the defined points in space at which an aircraft crosses from one environment to another.

CEPs may be “established” in that they are defined as part of the UAM Corridor itself. An example would be established points at either end of a UAM Corridor that are defined and disseminated as part of the UAM Corridor definition/description. They may also be “operation-defined,” which are those points in space on the boundary between the service environments (i.e., ATS and xTM [UAM]) along an accepted intent or trajectory that has not already been established.

Specific requirements or limitations regarding the use of CEPs may be addressed in applicable COPs and regulatory framework. Aircraft entering or exiting a UAM Corridor must meet the requirements of the airspace (e.g., Class B, C, D, E) they intended to use external to the UAM Corridor.

## 4.4.2 Conflict Management and Separation

Conflict management across the NAS includes the strategic activity of airspace organization and management. In certain situations, when operationally advantageous, UAM Corridors may enable UAM operations without traditional ATC services. Separation of operations within UAM Corridors may be provided through a layered approach of strategic and tactical deconfliction methods. Strategic deconfliction envisions the sharing of flight intent and the collaborative execution of the COPs relevant to deconfliction. In later stages, capabilities relying on V2V data exchanges guiding the execution of aircraft separation may also mature sufficiently for implementation.

When operating within a UAM Corridor, FAA regulations and COPs direct the manner of interactions across relevant actors for strategic and tactical deconfliction. UAM operators remain responsible for the safe conduct of operations, including operating relative to other aircraft, weather, terrain, and hazards and avoiding unsafe conditions. UAM separation is achieved via shared UAM Operational Intent, shared awareness, strategic deconfliction of flight intent, and the establishment of procedural rules.

While strategic deconfliction within UAM Corridors could occur during UAM Operational Intent planning, the need may remain for in-flight coordination, sharing, and tactical deconfliction. Initial analysis indicates strategic deconfliction in the planning phase may not be sufficient to support the operational tempo described as desired by industry. In the event a UAM aircraft operates outside of the bounds of shared UAM Operational Intent, notifications of the off-nominal event and updates to the UAM Operational Intent, if applicable, would be shared via the federated service network. Initial separation in UAM Corridors may leverage applicable VFR/IFR mechanisms (e.g., “see-and-avoid”). If aircraft technology and capabilities (e.g., equipage) evolve and mature, separation minima and AFRs may be introduced to provide higher capacity and support the projected increase in demand (i.e., operational tempo). The regulatory framework governing UAM operations would need to evolve significantly to account for the increasing levels of performance and automation. The maturation and implementation of both the advanced technologies and updated regulatory framework are coupled to changes in the separation minima and, by extension, the available throughput of a given UAM Corridor. The need for DCB capabilities or initiatives will be coupled to the pace at which the operational tempo increases and the envisioned advances in aircraft performance (e.g., equipage, capabilities) are realized.

## 4.4.3 Demand-Capacity Balancing (DCB)

DCB is applied when the requested resources cannot support the collective UAM Operational Intent demand. In certain circumstances, the excessive demand may not be due to UAM Corridor capacity but due to other factors such as congestion at origin or destination. Initial analysis of strategic deconfliction to eliminate tactical maneuvering identified that the operational tempo desired by UAM operators cannot be supported solely through strategic planning/deconfliction. The “buffer” necessary to account for uncertainty as the operational tempo increases leads to the eventual need for tactical deconfliction and DCB capabilities to optimize efficiency.

Within the UAM Corridor, flow management functions, including DCB, will be provided through Cooperative Flow Management (CFM) services. The business rules governing the execution of

CFM are included in relevant COPs, which are consistent with FAA authority including access, equity, safety, and security.

## 4.4.4 UAM Corridor Evolution

Initial UAM operations, characterized by low tempo and low complexity, will be executed using the current regulatory framework. As the tempo and complexity of operations increases, options available in the current regulatory framework (e.g., VFR corridors/flyways, T-routes) may accommodate the growth. As the operations continue to increase in volume and complexity, the implementation of simple UAM Corridors may become operationally advantageous for the airspace users and/or the ATS service providers. Initial UAM Corridors are expected to be “simple” in design (e.g., one-way UAM Corridors or single track in each direction), as illustrated in Figure 4. As UAM Corridors become more defined, AFR will likely be available, consistent with the evolving regulatory framework.

![9d081e5487013f5339043e7c888107e0607b9fc75d12498bff0b62dd98563929.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9d081e5487013f5339043e7c888107e0607b9fc75d12498bff0b62dd98563929.jpg)  
Figure 4: Early UAM Corridor Concept

With continued growth, UAM operational demand may result in exceeding a UAM Corridor’s initial design capacity, at which point increased capacity may be gained through additional structure including tracks and increased performance capabilities (e.g., ability to safely reduce separation minima within the UAM Corridor through improvements in navigation and/or other technologies). Additional options include variations in UAM Corridor topology to meet specific challenges such as “passing zones” as shown in Figure 5 and Figure 6. Note: An aircraft (and operator) meeting the performance requirements of a UAM Corridor as well as those of the surrounding airspace class (i.e., ATS environment) may elect to operate in whichever service environment they determine to be operationally advantageous.

![eba9471dd4795714d419612b1a5cc41eba89197f3093a524c4188114049bf59a.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/eba9471dd4795714d419612b1a5cc41eba89197f3093a524c4188114049bf59a.jpg)

Figure 5: Use of a Vertical Common Passing Zone  
![24baae0f946655336338bd184f0c31888598ce17bea02191fcb7e8b9289d5ffa.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/24baae0f946655336338bd184f0c31888598ce17bea02191fcb7e8b9289d5ffa.jpg)  
Figure 6: Use of Lateral Passing Zones

As the operational tempo and breadth of UAM aircraft physical performance (e.g., speed) continue to increase, Figure 7 depicts a notional internal UAM Corridor structure comprised of multiple “tracks.” The tracks reflect additional internal structure, which may also require increased performance requirements that support an increased operational tempo within the same UAM Corridor.

![7933ccfb1c51a30474381ed122373bbdc737b4fb3794e32b582dfa0b1f4a894b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7933ccfb1c51a30474381ed122373bbdc737b4fb3794e32b582dfa0b1f4a894b.jpg)  
Figure 7: UAM Corridor with Multiple Tracks

## 4.5 Weather and Obstacles Within the UAM Environment

PSUs or SDSPs support the UAM operator by supplying weather, terrain, and obstacle clearance data specific to the UAM operation. This data is accessed in the UAM Operational Intent planning phase to ensure strategic management of a UAM operation and updated in-flight, as appropriate. UAM operators monitor weather and winds prior to and throughout flight. If aircraft performance is inadequate to maintain required separation within the UAM Corridor, UAM operators are responsible to take appropriate action to ensure separation is maintained (e.g., do not take off, exit the UAM Corridor, operate per appropriate airspace rules).

## 4.6 Constraint Information and Advisories

UAM operators are responsible for identifying operational conditions or flight hazards that may affect an operation. This information is collected and assessed both prior to and during flight to ensure the safe conduct of the flight. PSUs support this UAM operator responsibility by supplying information and advisories including, but not limited to:

• Other airborne traffic including operations within and crossing UAM Corridors.

• Weather and winds.

Other hazards pertinent to low-altitude flight (e.g., obstacles such as a crane or powerline Notice to Air Missions (NOTAM), bird activity, local restrictions).

SAA status.

• UAM Corridor availability.

The sharing of projected demand and available capacity information between ATS and federated service network supports the applicable flow management function (e.g., TFM, CFM). Constraints may be shared from one environment to be complied with by the other, consistent with applicable procedures, COPs, and regulations.

## 5 Notional Architecture

Within the UAM cooperative management environment, the FAA would maintain regulatory and operational authority for airspace and traffic operations. UAM operations may be organized, coordinated, and managed by a federated set of actors through a distributed network that leverages interoperable information systems. Figure 8 depicts a notional architecture of the UAM actors and contextual relationships and information flows. This architecture is based on patterns established within the UTM architecture described in the UTM ConOps [2] and is consistent with the architecture described in the ETM ConOps [3].

The federated service network, comprised of individual PSUs operating as a collective, lies at the center of the UAM notional architecture and exchanges data with UAM operators, USSs, SDSPs, the FAA, and public interest stakeholders. PSUs receive supplemental data supporting UAM operation management from the SDSPs and provide relevant UAM operational data to the public. PSUs communicate and coordinate via the federated service network. This allows other UAM stakeholders (e.g., UAM operators, ATC, law enforcement) connected to a PSU to access data shared across the federated service network.

PSUs and USSs may exchange operational information about UAM and UTM operations in airspace under 400 feet where there is a potential need for cooperative separation (e.g., vertiports). Notionally, a USS can expand their service offerings to become a PSU and vice versa. Combined service providers may support operations in both the UAM and UTM environments. The architecture depicts the connectivity of the federated service network to USSs for information exchange while retaining a UAM-centric architectural view.

Vertiports exchange information with the federated service network to facilitate the communication of situational awareness and resourcing information to UAM operators. The PSUs make the aggregate vertiport information available for the operator to be aware of capacity and situational constraints present at the time of respective departure and arrival time. PSUs could potentially provide additional services with this information (e.g., suggested alternate vertiports, suggested alternate departure/arrival times).

The vertical dashed line in Figure 8 represents the demarcation between the FAA and industry responsibilities for the infrastructure, services, and entities that interact as part of UAM. The FAA-Industry Data Exchange Protocol provides an interface for the FAA to request UAM operational data on demand and send FAA information to the federated service network for distribution to UAM operators, PICs, UAM aircraft, and public interest stakeholders through the Service Security Gateway.

![770c7dea56349c92c13da84f5be7dc4aa741c5ecdc783f0421a6a7b6cbc98a4b.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/770c7dea56349c92c13da84f5be7dc4aa741c5ecdc783f0421a6a7b6cbc98a4b.jpg)  
Figure 8: Notional UAM Architecture

## 5.1 Supporting Services

UAM services that may be provided by PSUs and SDSPs are intended to be modular and discrete, allowing for increased flexibility in the design and implementation of new services. This modular approach would allow the FAA to provide tailored oversight of UAM operations and allows PSUs and SDSPs to provide focused services consistent with a business model and subscriber needs. Similar to UTM, UAM services may be characterized in one of the following ways.

1. Services that are required to be used by UAM operators due to FAA regulation or for a direct connection to FAA systems. These services must be qualified and approved by the FAA.

2. Services that may be used by a UAM operator to meet all or part of an FAA regulation. These services must meet an acceptable means of compliance and may be individually qualified and approved by the FAA.

3. Services that provide value-added assistance to a UAM operator but are not used for FAA regulatory compliance. These services may meet an industry standard but may not be qualified or approved by the FAA.

## 6 UAM Scenarios

This section provides high-level scenarios reflecting two operations. The first is conducted from departure to arrival within a UAM Corridor. The second operation departs a vertiport in the current Class B service environment (ATS), enters a UAM Corridor for a portion of the flight, exits back into Class B (ATS) and arrives at the vertiport. These scenarios further explore the UAM concept and each steps through phases of the flight’s operation, illustrating the operational and architectural information from Sections 4 and 5.

The scenarios demonstrate a subset of UAM operations and interactions during specific nominal operations. A nominal UAM operation is a single UAM operation that executes in accordance with the established performances, rules, policies, and procedures.

## 6.1 Nominal UAM Operation Completed Within a UAM Corridor

## 6.1.1 Planning Phase

Planning of this operation starts with the UAM operator receiving a request from an individual flight between Vertiport 1 and Vertiport 2.

The UAM operator obtains current conditions from the information provided by the subscribed PSU and relevant SDSP service. After determining that the current conditions are acceptable for the operation, the UAM operator submits desired UAM Operational Intent information (e.g., identifying information, vertiport locations, route of flight via UAM Corridor(s), desired time of operation) to the subscribed PSU.

The PSU, through the federated service network:

1. Evaluates the desired UAM Operational Intent against other operations that may cause a strategic conflict.

2. Evaluates UAM Operational Intent against known airspace constraints (e.g., FAA originating constraints, local restrictions).

3. Identifies availability of UAM Corridors and UAM vertiport resources.

Because there are no conflicting operations, airspace restrictions (e.g., Temporary Flight Restrictions [TFRs]), or vertiport resource limitations, the UAM operator’s desired UAM Operational Intent is considered strategically deconflicted and confirmed. The PSU notifies the UAM operator and provides the UAM Operational Intent to the federated service network.

The UAM operator considers possible modifications to the Operational Intent in the event of an off-nominal situation. The airspace classes and ATC facilities with jurisdiction for the airspaces that border the UAM Corridor(s) for the operation are identified. These prepare the PIC in case a contingency operation is required.

Most of the planning actions and information exchanges between the UAM operator and PSU are automated and expected to take very little time from the initial customer request to the confirmed UAM Operational Intent.

## 6.1.2 In-Flight Phases

Throughout all phases of flight, the UAM aircraft identification and location information are available to the UAM operator and subscribed PSU. The PIC and UAM operator monitor aircraft

performance to ensure nominal operation status is maintained. The PSU monitors Operational Intent conformance.

## 6.1.2.1 Departure Phase

The PIC departs from Vertiport 1 within the departure compliance window and enters the UAM Corridor.

## 6.1.2.2 En Route Phase

The PIC navigates along the UAM Corridor per the UAM Operational Intent. The UAM aircraft completes the en route portion of the flight per the UAM Operational Intent and approaches the arrival vertiport within the compliance window of the arrival time.

## 6.1.2.3 Arrival Phase

As the UAM aircraft approaches Vertiport 2, the PIC, UAM operator, PSU, and UAM vertiport confirm the landing pad is still available per the UAM Operational Intent. The PIC navigates to the allocated vertiport pad and lands the aircraft.

## 6.1.3 Post-Operations Phase

The UAM operator and PIC provide mission complete indication to the PSU. The PSU archives required UAM operational data per regulation.

## 6.2 Nominal UAM Operation Across Service Environments

This scenario describes a situation where a UAM operator plans a flight that departs from Vertiport 3, located in Class B airspace, and arrives at Vertiport 4, within Class B airspace, after using a UAM Corridor for transit. The operator enters and exits the UAM service environment through CEPs. Confirmed UAM Operational Intent is required for participation within the UAM environment. The UAM operators utilize a PSU who provides flight plan filing services.

## 6.2.1 Planning Phase

Planning of this operation starts with the UAM operator receiving a request from an individual customer for a flight between Vertiport 3 and Vertiport 4. The UAM operator obtains current conditions and vertiport availability from their subscribed PSU as well as relevant SDSP services (e.g., environment, situational awareness, strategic operational demand, supplemental data).

After determining the current conditions are acceptable for the operation, the UAM operator provides the necessary information to the PSU. In this case, the operation will use a UAM Corridor that traverses Class B airspace and operate within the Class B airspace to/from the UAM Corridor. In recognition of the cross-service environment operation, the operator’s information for the portion of the flight planned for the UAM Corridor includes the desired UAM Operational Intent information (e.g., identifying information, vertiport locations, route of flight via UAM Corridor(s), CEP locations, desired time of operation). As the operation, upon departure, will operate in Class B airspace, the operator also provides the PSU the required flight plan information for the ATS environment (e.g., flight ID, type of aircraft, route to CEP from departure vertiport, route from CEP to arrival vertiport). The PSU uses the flight plan information to coordinate with TFM and CFM services to secure clearance times and slot reservations for CEPs within the CA.

The subscribed PSU transmits the applicable information (e.g., flight information, flight plan) to the relevant ATS/xTM data exchange network as required by relevant regulations and COPs. The PSU receives information (e.g., ATC/TFM responses, notices, constraints) from the ATS data exchange portal for the UAM operator to use for situational awareness or to modify the planned intent/flight plan.

The PSU, through the federated service network:

1. Evaluates the desired UAM Operational Intent for other operations that may cause a strategic conflict.

2. Evaluates the UAM Operational Intent against known airspace constraints (e.g., FAA originating constraints, local restrictions).

3. Identifies availability of the UAM Corridor and UAM vertiport resources.

4. Receives any applicable flow management initiatives or constraints.

5. Files the flight plan from Vertiport 3 to Vertiport 4 through the UAM Corridor.

If there are no conflicting operations, airspace restrictions (e.g., TFRs), applicable flow management constraints (i.e., CFM and TFM), or vertiport resource limitations, the UAM operator’s desired UAM Operational Intent is considered strategically deconflicted and confirmed. The PSU notifies the UAM operator and provides the final UAM Operational Intent to the federated service network and flight plan information to the ATS exchange (e.g., Expect Departure Clearance Time [EDCT]).

Most of the planning actions and information exchanges (e.g., intent, flight plan filing) across the federated service network, ATS (i.e., ATC and TFM), operator, and PSU are automated and expected to take very little time from the initial customer request to the confirmed UAM Operational Intent and flight plan filing.

## 6.2.2 In-Flight Phases

Throughout all phases of flight (e.g., departure, en route, arrival) for a UAM operation, the UAM aircraft identification and location information are available to the UAM operator, ATC facility, and subscribed PSU. The PIC and UAM operator monitor aircraft performance to identify an offnominal state. The PSU monitors operational conformance to the confirmed UAM Operational Intents. Data exchange between CFM and TFM are monitored for accuracy and relayed to ATC and the PSU.

## 6.2.2.1 Departure Phase

Prior to departure, the PIC establishes two-way communication with the appropriate ATC facility to open the submitted flight plan that was submitted by the PSU. The PIC departs from Vertiport 3 within the departure compliance window, notifies the PSU (via automated departure acquisition), and enters Class B airspace. The UAM PIC monitors applicable ATC frequencies and complies with instructions while in Class B airspace. The UAM aircraft transitions into the UAM Corridor through the CEP submitted through the Operational Intent.

## 6.2.2.2 En Route Phase

The PIC navigates along the UAM Corridor per the confirmed UAM Operational Intent. The PIC deconflicts from other aircraft within the UAM Corridor with possible support from the UAM aircraft equipage or PSU services (e.g., flight data from active operations in the UAM Corridor). Flight status is monitored by CFM to TFM and updated as necessary within the system. The UAM aircraft completes the en route portion of the flight per the UAM Operational Intent and approaches the CEP within the compliance window of the arrival time.

## 6.2.2.3 Arrival Phase

Prior to arriving at the submitted CEP to exit the UAM Corridor into Class B airspace, the data exchange (e.g., handoff) is activated to ATC and frequency change is conducted. The UAM PIC establishes two-way communication and positive clearance with the appropriate ATC facility. The UAM aircraft enters Class B airspace through the CEP per ATC instruction.

As the UAM aircraft approaches Vertiport 4, the PIC, UAM operator, PSU, and UAM vertiport confirm the landing pad is still available per the UAM Operational Intent. The PIC navigates to the allocated vertiport pad and lands the aircraft.

## 6.2.3 Post-Operations Phase

The UAM operator/PIC provides mission completion indication to the PSU and the ATC facility.   
The PSU archives required UAM operational data.

## 7 UAM Evolution

The UAM ConOps 2.0 reflects FAA efforts, in collaboration with NASA, industry, and other stakeholders, to advance UAM. It begins with the introduction of low-complexity, low-operational tempo operations leveraging the current regulatory framework (e.g., VFR, IFR) and building toward higher operational tempo with the institution of UAM airspace structures (i.e., UAM Corridors) where and when operationally advantageous, using a performance-based construct.

As operations occur and experience is gained, the concept may mature and evolve as the FAA continues to engage stakeholders for their perspectives on new technologies, techniques, and automation, both ground-based and airborne, to identify those most capable of addressing the evolving challenges and opportunities. This evolutionary approach to UAM could provide advantages. By initially supporting lower complexity operations, implementation can be streamlined to the environment using current capabilities that meet performance requirements and do not require full-scale regulatory and operational infrastructure changes. Incremental changes to the regulatory framework, “hard” infrastructure (e.g., systems and vertiports), and “soft” infrastructure (e.g., processes and procedures) could help support the UAM operational demand and complexity as they increase in concert with other cooperative environments, such as UTM and AAM. These incremental changes may also support the progression of the existing ATS system, maintaining fair and equitable access to airspace across the full airspace user community.

## Appendix A References

[1] International Civil Aviation Organization (ICAO), Document 9854, Global Air Traffic Management Operational Concept (GATMOC), First Edition, 2005.

[2] FAA, Unmanned Aircraft System (UAS) Traffic Management (UTM) Concept of Operations (ConOps) Version 2.0. 2020.

[3] FAA, Upper Class E Traffic Management (ETM) Concept of Operations (ConOps) Version 1.0. 2020.

## Appendix B Acronyms

All acronyms used throughout the document are provided in Table 1.

Table 1: Acronyms
<table><tr><td>Acronym</td><td>Definition</td></tr><tr><td>AAM</td><td>Advanced Air Mobility</td></tr><tr><td>AFR</td><td>Automated Flight Rule</td></tr><tr><td>ATC</td><td>Air Traffic Control</td></tr><tr><td>ATS</td><td>Air Traffic Services</td></tr><tr><td>CA</td><td>Cooperative Area</td></tr><tr><td>CBR</td><td>Community Business Rule</td></tr><tr><td>CEP</td><td>Corridor Entry/Exit Point</td></tr><tr><td>CFM</td><td>Cooperative Flow Management</td></tr><tr><td>CNS</td><td>Communication, Navigation, and Surveillance</td></tr><tr><td>COP</td><td>Cooperative Operating Practice</td></tr><tr><td>ConOps</td><td>Concept of Operations</td></tr><tr><td>DCB</td><td>Demand-Capacity Balancing</td></tr><tr><td>DEP</td><td>Distributed Electric Propulsion</td></tr><tr><td>DOT</td><td>Department of Transportation</td></tr><tr><td>EDCT</td><td>Expect Departure Clearance Time</td></tr><tr><td>ETM</td><td>Upper Class E Traffic Management</td></tr><tr><td>eVTOL</td><td>Electric Vertical Takeoff and Landing</td></tr><tr><td>FAA</td><td>Federal Aviation Administration</td></tr><tr><td>G/G</td><td>Ground-to-Ground</td></tr><tr><td>HOTL</td><td>Human-on-the-Loop</td></tr><tr><td>HOVTL</td><td>Human-Over-the-Loop</td></tr><tr><td>HWTL</td><td>Human-Within-the-Loop</td></tr><tr><td>IFR</td><td>Instrument Flight Rules</td></tr><tr><td>IMC</td><td> Instrument Meteorological Conditions</td></tr><tr><td>LOA</td><td>Letter of Agreement</td></tr><tr><td>MRO</td><td>Maintenance, Repair, and Overhaul</td></tr><tr><td colspan="1" rowspan="1">NAS</td><td colspan="1" rowspan="1">National Airspace System</td></tr><tr><td colspan="1" rowspan="1">NASA</td><td colspan="1" rowspan="1">National Aeronautics and Space Administration</td></tr><tr><td colspan="1" rowspan="1">NOTAM</td><td colspan="1" rowspan="1">Notice to Air Missions</td></tr><tr><td colspan="1" rowspan="1">PIC</td><td colspan="1" rowspan="1">Pilot in Command</td></tr><tr><td colspan="1" rowspan="1">PSU</td><td colspan="1" rowspan="1">Provider of Services for UAM</td></tr><tr><td colspan="1" rowspan="1">RPIC</td><td colspan="1" rowspan="1">Remote Pilot in Command</td></tr><tr><td colspan="1" rowspan="1">SAA</td><td colspan="1" rowspan="1">Special Activity Airspace</td></tr><tr><td colspan="1" rowspan="1">SDSP</td><td colspan="1" rowspan="1">Supplemental Data Service Provider</td></tr><tr><td colspan="1" rowspan="1">TFM</td><td colspan="1" rowspan="1">Traffic Flow Management</td></tr><tr><td colspan="1" rowspan="1">TFR</td><td colspan="1" rowspan="1">Temporary Flight Restriction</td></tr><tr><td colspan="1" rowspan="1">UAM</td><td colspan="1" rowspan="1">Urban Air Mobility</td></tr><tr><td colspan="1" rowspan="1">UAS</td><td colspan="1" rowspan="1">Unmanned Aircraft Systems</td></tr><tr><td colspan="1" rowspan="1">USS</td><td colspan="1" rowspan="1">UAS Service Supplier</td></tr><tr><td colspan="1" rowspan="1">UTM</td><td colspan="1" rowspan="1">UAS Traffic Management</td></tr><tr><td colspan="1" rowspan="1">V2V</td><td colspan="1" rowspan="1">Vehicle-to-Vehicle</td></tr><tr><td colspan="1" rowspan="1">VFR</td><td colspan="1" rowspan="1">Visual Flight Rules</td></tr><tr><td colspan="1" rowspan="1">VMC</td><td colspan="1" rowspan="1">Visual Meteorological Conditions</td></tr><tr><td colspan="1" rowspan="1">VTOL</td><td colspan="1" rowspan="1">Vertical Takeoff and Landing</td></tr><tr><td colspan="1" rowspan="1">xTM</td><td colspan="1" rowspan="1">Extensible Traffic Management</td></tr></table>

## Appendix C Glossary

Table 2 provides a glossary of UAM terms used throughout this ConOps. These terms are in addition to those defined in Section 1.4, which provides terms key to establishing the context of the UAM concept.

Table 2: Glossary
<table><tr><td colspan="1" rowspan="1">Acronym</td><td colspan="1" rowspan="2">DefinitionThe terms "advanced air mobility” and “AAM'"' mean atransportation system that transports people and property by airbetween two points in the United States using aircraft with advancedtechnologies, including electric aircraft or electric vertical take-offand landing aircraft, in both controlled and uncontrolled airspace.</td></tr><tr><td colspan="1" rowspan="1">Advanced AirMobility (AAM)</td></tr><tr><td colspan="1" rowspan="1">Conflict</td><td colspan="1" rowspan="1">Any situation involving aircraft and hazards in which the applicableseparation minima may be compromised [1].</td></tr><tr><td colspan="1" rowspan="1">Constraint</td><td colspan="1" rowspan="1">An impact to the capacity or use of a resource preferred by anoperator, defined with time and geographically specified airspaceinformation. A constraint may restrict access to airspace foroperations or may be advisory in nature.</td></tr><tr><td colspan="1" rowspan="1">CooperativeSeparation</td><td colspan="1" rowspan="1">Separation based on shared flight intent and data exchanges betweenoperators, stakeholders, and service providers. Cooperativeseparation is supported by defined COPs as well as applicable rules,regulations, and policies.</td></tr><tr><td colspan="1" rowspan="1">Demand-CapacityBalancing (DCB)</td><td colspan="1" rowspan="1">Strategic evaluation of system-wide traffic flows and aerodromecapacities to allow airspace users to determine when, where, and howthey operate, while mitigating conflicting needs for airspace andaerodrome capacity. This collaborative process allows for theefficient management of air traffic flow through the use of information on system-wide air traffic flows, weather, and assets [1].</td></tr><tr><td colspan="1" rowspan="1">Human-on-the-Loop(HOTL)</td><td colspan="1" rowspan="1">Human supervisory control of the automation (i.e., systems) where the human actively monitors the systems and can take full controlwhen required or desired.</td></tr><tr><td colspan="1" rowspan="1">Human-Over-the-Loop (HOVTL)</td><td colspan="1" rowspan="1">Human informed, or engaged, by the automation (i.e., systems) to take actions. Human passively monitors the systems and is informedby automation if, and what, action is required. Human is engaged bythe automation either for exceptions that are not reconcilable or aspart of rule set escalation.</td></tr><tr><td colspan="1" rowspan="1">Human-Within-the-Loop (HWTL)</td><td colspan="1" rowspan="1">Human is always in direct control of the automation (systems).</td></tr><tr><td colspan="1" rowspan="1">Acronym</td><td colspan="1" rowspan="1">Definition</td></tr><tr><td colspan="1" rowspan="1">Operational Intent</td><td colspan="1" rowspan="1">Also referred to as operation intent, the future operational positioninformation, consisting of spatial and temporal elements, that isexchanged between xTM operators to support cooperative trafficmanagement.</td></tr><tr><td colspan="1" rowspan="1">Operational Tempo</td><td colspan="1" rowspan="1">The density, frequency, and complexity of operations.</td></tr><tr><td colspan="1" rowspan="1">Provider of Servicesfor UAM (PSU)</td><td colspan="1" rowspan="1">An entity that assists UAM operators with meeting UAM operationalrequirements to enable safe and efficient use of UAM Corridors andvertiports. This service provider shares operational data withstakeholders and confirms flight intent.</td></tr><tr><td colspan="1" rowspan="1">StrategicDeconfliction</td><td colspan="1" rowspan="1">The process of arranging, negotiating, and prioritizing OperationalIntent (e.g., volumes, routes, trajectories, time assignments) ofaircraft to minimize the likelihood of airborne conflicts betweenoperations.</td></tr><tr><td colspan="1" rowspan="1">Tactical Deconfliction</td><td colspan="1" rowspan="1">The process of executing one or more actions to avoid an airborneconflict in a timely manner when strategic deconfliction has failed orwas not executed.</td></tr><tr><td colspan="1" rowspan="1">UAS TrafficManagement (UTM)</td><td colspan="1" rowspan="1">The manner in which the FAA will support operations for UASoperating in low-altitude airspace.</td></tr></table>

# FAA AAM Implementation Plan (I28)

![dc0f690b3735eafdcead37afc9465b30d7a59a76ed803450ea84b82a9575609c.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/dc0f690b3735eafdcead37afc9465b30d7a59a76ed803450ea84b82a9575609c.jpg)

## Advanced Air Mobility (AAM) Implementation Plan

Near-term (Innovate28) Focus with an Eye on the Future of AAM Version 1.0 / July 2023

![7918a040f7a792905cb464f3972ef21b242802451a34ceaadd1fc6c77d599452.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/7918a040f7a792905cb464f3972ef21b242802451a34ceaadd1fc6c77d599452.jpg)

PAGE INTENTIONALLY BLANK

## Table of Contents

1 Advanced Air Mobility... . 1   
1.1 AAM Definition .. . 1   
1.2 AAM Integration into the National Airspace System... .. 1   
1.3 Stakeholder Collaboration . .. 2   
2 Introduction to Innovate28 .... ... 5   
3 Implementation Plan Overview .... .. 6   
4 Innovate28 Key Site Operations.. .. 7   
4.1 AAM Aircraft ....... ... 7   
4.2 AAM Operations..... ..... 8   
4.3 I28 Scenario.... . 13   
5 Innovate28 Workstreams.. . 15   
5.1 Certification ..... ... 15   
5.2 Operational Suitability .. . 15   
5.2.1 Operations Certification . . 16   
5.2.2 Aircraft Certification... . 18   
5.3 Airspace and Air Traffic Management.. . 20   
5.4 Infrastructure.... . 22   
5.4.1 Existing Infrastructure . . 22   
5.4.2 New Infrastructure... .. 23   
5.4.3 Vertiport-Related Research . .. 23   
5.4.4 Vertiport Standards and Oversight. . 24   
5.5 Environment... .. 25   
5.6 Hazardous Materials Safety ... . 26   
5.7 Community Engagement... . 27   
6 Innovate28 Integrated Schedule .... . 28   
7 AAM Evolution Framework.... . 31

## List of Figures

Figure 1. Integrated Master Schedule Version 1.0......... .. 29

## List of Tables

Table 1. Detailed List of Activities in the Integrated Master Schedule Version 1.0 30   
Table 2. AAM Coordination Areas... .. 32   
Table 3. AAM Maturity Levels.. . 33

## 1 Advanced Air Mobility

Transportation is constantly evolving, and each step forward yields new opportunities that fundamentally change how people and goods are being transported. A new era of aviation once only portrayed in movies or science fiction is taking off. Advanced Air Mobility (AAM) is an emerging aviation ecosystem that leverages new aircraft and an array of innovative technologies to provide the opportunity for more efficient, more sustainable, and more equitable options for transportation.

![4732d0513b03ca041ac209a4739d8d53b88239fb85842ca09cd517bcf719e23f.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4732d0513b03ca041ac209a4739d8d53b88239fb85842ca09cd517bcf719e23f.jpg)

## 1.1 AAM Definition

As defined in the AAM Coordination and Leadership Act (P.L. 117-203, 136 Stat. 2227), October 17, 2022, “AAM is a transportation system that moves people and property by air between two points in the United States (U.S.) using aircraft with advanced technologies, including electric aircraft, or electric vertical takeoff and landing (eVTOL) aircraft, in both controlled and uncontrolled airspace.” For purposes of this Implementation Plan, however, the scope of AAM is limited to those engaging in passenger-carrying or cargo operations with a pilot on board.

## 1.2 AAM Integration into the National Airspace System

The Federal Aviation Administration (FAA) has a long, successful history of bringing new technologies safely into aviation. The agency’s role in integrating AAM into the National Airspace System (NAS) is to ensure this new generation of aircraft maintains the highest level of operational safety that defines commercial aviation today. The FAA’s top priority and statutory responsibility are to ensure the safety of the traveling public. The agency is looking at every necessary aspect to support AAM flights: the aircraft itself, the framework for operations, access to the airspace, operator training, infrastructure development, environmental impacts, and community engagement.

As these aircraft are being developed, the FAA will amend, as appropriate, operational rules and pilot training requirements. Longer term, the agency will develop permanent regulations to safely enable powered lift operations and pilot training and certification.

![d5d2fd1750cb198e2b581d0a509316a2902a27c265c815ba611b896935585ab3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d5d2fd1750cb198e2b581d0a509316a2902a27c265c815ba611b896935585ab3.jpg)

## The FAA is implementing a crawl-walk-run

methodology that recognizes early opportunities to support Entry into Service (EIS) operations through existing services and infrastructure with minimal changes. The agency is doing this while developing a path to implementation of more advanced concepts and capabilities to support increasing scale and automation of AAM operations, as well as integration with other types of aircraft operating in the NAS.

To address the development of a near-term ecosystem, the FAA created Innovate28 (I28), a joint government and industry initiative that will culminate in integrated AAM operations at one or more key site locations by the 2028 timeframe. The FAA also recognizes and has begun executing the collaborative actions needed to mature AAM concepts, operations, and regulatory frameworks beyond initial operations and into the mid-term and mature state phases (see Section 7). This Implementation Plan shows how the agency expects all these pieces to come together to allow the industry to scale safely.

## 1.3 Stakeholder Collaboration

Operationalizing AAM in the NAS and establishing timelines from EIS to operations at scale requires collaboration with, and commitments by, many stakeholders to ensure safe, efficient, and equitable operations, including:

## Federal Aviation Administration

From a federal level, the FAA has sole and exclusive authority over all aviation safety aspects of AAM integration, including operating rules, aircraft certification, and pilot certification. The agency provides a leadership role in identifying and integrating the responsibilities of all the key actors and stakeholders. The FAA develops and processes all certification, policy and procedures, rulemaking, and regulatory activities to ensure safety of flight, and strives to ensure that industry (including original equipment manufacturers (OEMs), aircraft operators, and vertiport operators) and local, state, and tribal governments can accommodate AAM operations and plan accordingly.

In support of I28, the FAA established internal workstreams, called iTeams. These teams are dedicated to addressing major focus areas for AAM integration, including Certification, Airspace and Air Traffic Management, Infrastructure, Environment, Hazardous Materials Safety, and Community Engagement, to ensure a coordinated approach for I28 operations.

## Other Government Agencies

The FAA is leveraging existing programs and research conducted by other government agencies to integrate AAM more rapidly into the NAS, including the National Aeronautics and Space Administration (NASA), U.S. Department of Transportation (DOT), Department of Defense, and others. For example, through the FAA’s extensive AAM-focused partnership with NASA’s AAM Program and the National Campaign and collaboration with the U.S. Air Force AFWERX Prime programs, the FAA is able to leverage the research, data, and testing experience in the shared mission to safely integrate AAM aircraft.

In addition to collaboration at the federal level, the FAA is engaging with local, state, tribal, and territorial governments that have vested interests in making decisions to ensure safe and successful AAM operations from local and regional planning, power infrastructure, intermodal transportation, and community perspectives. These entities will likely be responsible for the coordination, logistics, zoning, licensing of infrastructure, and the community engagement necessary to support AAM operations.

## Inter-Agency Working Groups

The FAA participates in several inter-agency AAM groups, including the DOT AAM Interagency Working Group, which was established by the AAM Coordination and Leadership Act. Much like the FAA iTeams’ structure, the DOT AAM Interagency Working Group is coordinating efforts related to safety, operations, infrastructure, physical security and cybersecurity, and federal investment necessary for maturation of the AAM ecosystem in the U.S. They are focused on ensuring cohesive and consistent Executive Branch-wide policy through a collaborative and proactive approach that supports the FAA’s integration of AAM into the NAS.

The FAA also participates in the newly-formed International Civil Aviation Organization (ICAO) AAM Study Group. The 41st ICAO Assembly recognized that the rapidly evolving AAM ecosystem requires a globally harmonized operational and regulatory framework and guidance. ICAO provides the forum for 26 international stakeholders to develop a holistic vision and framework to achieve global harmonization and interoperability of AAM implementation, allowing all countries to benefit from the AAM operations. The FAA and other government agencies participate in all relevant ICAO technical panels that will ultimately work on international standards and recommended practices for AAM as the specific work is forwarded for their action from the AAM Study Group.

## AAM Operators and Manufacturers

Companies developing or operating AAM aircraft are key stakeholders in the integration process. These companies will need to work with government agencies to bring forward the use cases and locations of interest, obtain necessary certifications and approvals, and ensure that their aircraft and operations meet safety and regulatory requirements. They will also need to consider the environmental impacts of their aircraft and operations, engage with relevant communities, and minimize environmental and other impacts on communities.

## Infrastructure Providers

Any time new transportation is introduced, communities must plan for the integration of those operations either within existing infrastructure or through the development of new facilities. Companies that provide charging stations, vertiports, and other infrastructure necessary for AAM operations will also play a role in integration. Providers of private infrastructure that do not require FAA approval will, in particular, need to engage with relevant communities, minimize environmental and other impacts on communities, and foster community support.

## Communities and the Public

As AAM aircraft begin to operate in urban areas, communities and the general public will be affected by these new technologies, capabilities, and services. Community involvement is the process of engaging in dialogue and collaboration with communities affected by FAA actions. This process supplements the public involvement activities required under other laws or requirements. Public engagement and education through involvement of all stakeholders will be necessary to ensure that communities understand the benefits and impacts of AAM operations, and to address any concerns they may have. The AAM industry offers the prospects of convenient alternatives to traditional transportation, as well as increased access to air transportation. However, for this emerging industry to reach its fullest potential, it must gain the support of the general public. The FAA encourages communities to get involved now in these early phases, and to stay engaged.

## 2 Introduction to Innovate28

![71250a893a77ab786b391cf3e91add6ba0c0cc4f0e8aa5d2fb042ee525f91bb3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/71250a893a77ab786b391cf3e91add6ba0c0cc4f0e8aa5d2fb042ee525f91bb3.jpg)

On May 3, 2023, the FAA released Version 2.0 of the Urban Air Mobility (UAM) Concept of Operations (ConOps) that describes the technical roadmap for enabling UAM, which is an urban-focused subset of AAM, from the near-term to far-term. The focus of this Implementation Plan, Version 1.0, is to document the work required to enable initial AAM operations in a variety of operational settings or “key sites” in the near-term.

## Initial Integration of AAM Operations at One or More Key Sites

Innovate28 (I28) is an FAA initiative that will culminate in integrated AAM operations with OEMs and/or operators flying between multiple origins and destinations at one or more locations in the U.S. by 2028. I28 marks one milestone on the AAM evolutionary continuum and the path to full integration and operations at scale across the NAS. I28 will leverage public-private partnerships to identify key locations and use cases of interest to AAM industry stakeholders while promoting an all-hands-on deck approach to ensure the necessary steps are taken to enable these operations. Leveraging lessons learned from OEMs and/or operators conducting individual EIS building block operations, I28 operations are expected to be larger in scale than initial EIS operations. I28 is intended to result in “leave behind” processes, infrastructure, procedures, and local knowledge at the key site(s). Additionally, the collective experience gained through the I28 initiative is expected to support expanded operations in other areas of the country.

## Repeatable Implementation Methodology

The I28 implementation approach includes documenting steps and protocols and collecting data over the course of the effort to develop a repeatable methodology, including processes, procedures, and mechanisms, for expanding AAM operations to other locations across the NAS. This methodology will be used as a guide for future sites to collaborate with the FAA and other stakeholders to streamline implementation of AAM solutions. The FAA will also leverage the I28 efforts, as well as the EIS building blocks, in its ongoing work to evolve and advance AAM into the future.

## 3 Implementation Plan Overview

This AAM Implementation Plan is a living document that will guide implementation efforts and mature as the FAA works with stakeholders to refine and execute AAM implementation strategies. It will be updated periodically to reflect the continued plans and progress with AAM integration, roadmaps, and schedules for I28 and beyond as work continues to advance towards the mature state vision of AAM operations across the NAS.

Version 1.0 provides details for the near-term I28 initiative, which will enable a repeatable AAM ecosystem at key locations based on information known to date. The evolution of AAM beyond I28 is also previewed. Version 1.0 specifically addresses the following:

![aa5dd90e6fdd681c577e9f8569f6e0be316fe8edc27e0d94c3d6455ca9756da3.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/aa5dd90e6fdd681c577e9f8569f6e0be316fe8edc27e0d94c3d6455ca9756da3.jpg)

## • I28 Key Site Operations

o Description of the operating environment in 2028 based on assumptions and expectations of AAM aircraft and operations, including a scenario thread for a generic key site location

o Overarching framework that FAA stakeholders can use to identify and work through key challenge areas, executing to a common vision

## I28 Workstreams

o Holistic approach to the required efforts, both internal and external to the FAA, needed to meet I28 goals (presented in Section 2)

O Descriptions of work completed to date and gaps to be addressed in Certification, Airspace and Air Traffic Management, Infrastructure, Environment, Hazardous Materials Safety, and Community Engagement

## I28 Integrated Master Schedule

o Detailed schedule across workstream focus areas that supports I28 operations and leave behind processes

o Tool for tracking the milestones of internal and external stakeholders (e.g., tribal/state/local government, and industry) who manage their own activities relevant to implementation at specific site(s)

## • AAM Evolution Framework

o High-level view of the evolution of AAM operations and an associated framework for the continued development and commitments that are needed to advance AAM integration in the NAS

## 4 Innovate28 Key Site Operations

The I28 initiative envisions a near-term AAM operational ecosystem that has advanced from EIS at various locations to substantive presence at locations of interest. Since AAM aircraft are currently undergoing or are being planned to undergo the certification process, and specific operational needs are still being defined, it is necessary to make assumptions as to how the AAM industry will operate and what the supporting capabilities will be in 2028. The I28 key site operations presented here are based on industry and FAA projections on the state of technology development, air and ground supporting infrastructure and services, and other capabilities. These assumptions will continue to be updated in future versions of this document as the industry advances and regulations are developed.

The following addresses the assumptions and expectations about AAM aircraft with respect to certification and operating characteristics. I28 AAM operations are then described in the context of the operating environment, including flight operations, airspace usage and route structure, air traffic control (ATC) services, and infrastructure. A scenario thread is also presented for an I28 AAM operation.

## 4.1 AAM Aircraft

For I28, AAM aircraft will be authorized for piloted operations and will transport passengers and/or cargo within the limits of the aircraft and certification regulations. The aircraft are expected to range in size from single passenger to larger occupancy shuttles, and employ new means of propulsion (e.g., electric motors, hydrogen fuel, hybrid designs). Many are capable of vertical takeoff and landing (VTOL) or short takeoff and landing (STOL) operations and quickly transition to fixed-wing operation after takeoff. It is assumed wake characteristics will be known, including the impacts of wake from other aircraft on AAM

![943feb4d1157fe561bb8798751a27163cd232607e922e893c860ae527f23a9e1.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/943feb4d1157fe561bb8798751a27163cd232607e922e893c860ae527f23a9e1.jpg)

aircraft and an AAM aircraft’s own wake generation.

AAM aircraft are expected to be type certificated as special class under 14 Code of Federal Regulations (CFR) § 21.17(b). Because these aircraft have novel airframes and powerplants, the FAA is using many of the performance-based regulations in 14 CFR part 23, Airworthiness Standards: Normal Category Airplanes, for the certification basis. AAM commercial operators are expected to be certified to operate under 14 CFR part 135, Operating Requirements: Commuter and on Demand Operations and Rules Governing Persons on Board Such Aircraft. Pilots of powered lift aircraft are expected to be rated (type rated as required) for each powered lift aircraft they fly, and they will be required to meet updated qualification requirements for operating under part 135.

AAM aircraft are expected to operate under part 135, including seeking FAA approval for the carriage of dangerous goods and hazardous materials, consistent with the aircraft’s type certificated operating weight to include passenger carriage or cargo capability and their frequency of

![4feda8719ce6f195c5a9ce9309cb0914b1abdd881fb6d6bdc731597eafccba87.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/4feda8719ce6f195c5a9ce9309cb0914b1abdd881fb6d6bdc731597eafccba87.jpg)

operations. These operations must be part of the operator’s FAA approved Dangerous Goods program and further authorized within the operator’s Operations Specifications.

## 4.2 AAM Operations

The descriptions of I28 AAM operations in this section are agnostic to location. As key sites are identified, site-specific airspace and air traffic management (ATM) solutions will be developed for operations within defined geographical areas based on AAM operator use cases.

## Airspace Usage and Route Structure

AAM operators are expected to comply with existing communication, navigation, and surveillance (CNS) requirements for the airspace in which they will operate. For I28, the expectation is that the aircraft will operate from the surface to 4000’ above ground level in urban and metropolitan areas, and in relatively close proximity to or directly on airports. This means that AAM aircraft will operate predominately in or around Class B and C airspace.

To operate within Class B airspace, pilots must receive ATC clearance, and aircraft are required to be equipped with an operating two-way radio, Automatic Dependent Surveillance – Broadcast (ADS-B) Out, suitable navigation capability, and an operable transponder with altitude reporting capability. Initial AAM aircraft operations are generally expected to operate in compliance with Visual Flight Rules (VFR) weather minima in visual meteorological conditions (VMC).

VFR aircraft operating within Class B airspace receive separation services from ATC. VFR aircraft may obtain an ATC clearance to transit Class B airspace, if needed, however, the FAA encourages VFR pilots to operate above or below, or transit Class B airspace using established VFR corridors. To operate within Class C airspace, pilots must initiate twoway radio communications prior to entry and maintain communications while in the airspace. They must also be equipped with a two-way radio and an operable transponder with altitude reporting capability.

The addition of AAM operations will add to the already busy traffic levels of Class B and C airspace. In cases where existing VFR procedures do not meet the needs of air traffic facilities or AAM operators, special agreements or coordination may need to occur to accommodate the increase in traffic levels. Ideally, agreements made at the local level will reduce ATC workload.

Charted routes will be the primary routing structure used by AAM aircraft. This approach enables the FAA to develop routes that accommodate AAM operator needs while leveraging the existing design and charting processes. The development of airspace route structures for I28 operations will consider design standards based on 14 CFR parts 135 and 91, General Operating and Flight Rules, local procedures, terrain, and traffic flows. Pilot adherence to charted I28 routes and the recommended

![d36395ec16b471db9d6f06c9ab149cc068d2237c9a80eda071ef17a8add4b6a2.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/d36395ec16b471db9d6f06c9ab149cc068d2237c9a80eda071ef17a8add4b6a2.jpg)

altitudes or flight ceilings associated with them are voluntary. However, ATC may assign charted routes and altitudes where pilot compliance is required, provided such procedures are called for in specific FAA-operator Letters of Agreement (LOAs), or are necessitated by traffic density and/or safety considerations. ATC may also restrict operations within designated operating zones when certain criteria are met, and as requested by the appropriate authorities. Noise and other environmental considerations are accounted for in the airspace design. Changes to airspace design and/or new routes will likely require the FAA to conduct environmental review and community outreach.

I28 AAM routes will be designed for use in VFR conditions only, and where possible, use existing or modified low altitude VFR routes and constructs. While these routing constructs do not inherently provide separation or segregation of participating AAM traffic, they are developed to assist pilots in avoiding major controlled traffic flows. The routes1 may include:

VFR flyways - General flight paths not defined as a specific course, for use by pilots in planning flights into, out of, through or near complex terminal airspace to avoid Class B airspace. An ATC clearance is not required to fly these routes.

VFR corridors - Airspace through Class B airspace, with defined vertical and lateral boundaries, in which aircraft may operate without an ATC clearance or communication with ATC.

VFR transition routes - Specific flight courses depicted on a terminal area chart for transiting a specific Class B airspace. These routes include specific ATC‐assigned altitudes, and pilots must obtain an ATC clearance prior to entering Class B airspace on the route.

Special flight rule areas - Airspace of defined dimensions, above land areas or territorial waters, within which the flight of aircraft is subject to the rules set forth in 14 CFR Part 93, unless otherwise authorized by ATC.

I28 AAM routes may include non-published routes. They may also require development of new routes. More information is needed to make this determination; it may be a combination of existing and new route structures until a specific AAM route process can be developed. It is important to note, however, that no unique AAM airspace structures (e.g., dedicated AAM airspace corridors) or procedures are expected to be implemented by this 2028 timeframe.

Efforts will be made when developing and designating AAM routes to ensure, to the extent possible, that the flow of AAM traffic does not negatively impact or interfere with other air traffic flows or other airspace available to ATC today. In some cases, this may be unavoidable, and operational efficiency will need to be considered. As previously noted, these routing constructs do not inherently provide separation or segregation of AAM traffic, therefore see-and-avoid will continue to be the primary means of aircraft separation.

## Air Traffic Control Services

For I28, ATC services will be provided to AAM operators as needed or required and are defined in FAA regulations, directives, and agreements (e.g., FAA Order Joint Order (JO) 7110.65, Air Traffic Control, LOAs, Memorandums of Understanding (MOU), Notices to Air Missions (NOTAM), and Advisory Circulars (AC)). AAM operations may require an LOA covering local procedures or routes, establishment of reserved discrete beacon codes, and use of abbreviated call signs.

The following lists the expectations of ATC and OEMs/operators with respect to operations at designated key site locations.

AAM operators comply with the appropriate CFR pertaining to ATC or apply for a waiver/exemption.

AAM operations are expected to be conducted with flight schedules that are predetermined. Schedules are provided in advance of operations and coordinated with local ATC and all other identified stakeholders.

• The pilot has two-way radio communication with ATC when required.

VFR aircraft operating within Class B airspace receive mandatory traffic advisories and safety alerts, as well as separation services where required.

VFR aircraft operating in Class C airspace receive sequencing services and ATC separates IFR aircraft from the VFR aircraft. VFR aircraft receive traffic advisories and safety alerts. VFR pilots retain responsibility for their separation.

In other airspace, ATC provides oversight with traffic advisories and safety alerts, but the pilot is responsible for separation.

AAM aircraft operators are not guaranteed ATC flight following services outside of Class B, C, or D airspace where mandatory air traffic services are not required.

Air traffic automation is as it currently exists.

o There are no expected major changes to ATC automation systems within the 2025 to 2028 timeframe to support I28 operations.

Third-party service providers may support non-safety critical aspects of operations (e.g., operator scheduling of flights), but not substitute for ATC services where required by rule.

Existing communication methods are used for pilot-controller communications for AAM VFR operations.

## Infrastructure

Initial AAM operations in the 2025-2028 timeframe are expected to primarily use existing airports and heliports (with modification where required to meet FAA’s interim guidance for vertiport design). Greenfield or infill (repurposed) development for new vertiports is also expected to connect operations to destinations near a city center or other preferred locations. It is unlikely, but possible, that specially built vertiports will be available in this timeframe. Modifications may be required for existing ground and air infrastructure due to the nature of these new aircraft. For example, if heliports are used as vertiports, they require the following infrastructure to successfully operate in the 2025-2028 time:

Adequate AAM aircraft parking zones for loading/unloading. An efficient vertiport has parking zones that are separate from the “pad” that is used for takeoff and landing. Separate parking zones allow for safe entrance and egress of passengers. They also allow for parking of vehicles waiting for demand to materialize.

Infrastructure sizing, dimensional geometry and load bearing requirements modified to comply with FAA Engineering Brief (EB) #105, Vertiport Design (September 21, 2022). The dimensional and sizing requirements for vertiport landing and safety areas may warrant differences from heliports based on the design and performance characteristics of AAM aircraft.

Charging stations. Safe rapid charging stations for electric batteries are present at vertiports as well as adequate cooling stations and hazardous materials (HazMat) lockers/storage for batteries and fire suppression for battery fires. Sufficient amperage is available to reduce recharging time to the minimum.

Weather station. The vertiport has a weather station, possibly an Automated Surface Observing System (ASOS) or Automated Weather Observing System (AWOS), if it is remote from an airport. AAM pilots need to know wind speed and direction, as well as visibility, when planning an arrival or departure. Vertiports co-located with an airport can use the airport’s weather system.

Fire management services. The vertiport has access to fire management services with personnel trained in handling electric/hydrogen fueled fires.

New vertiport facilities follow the guidance in FAA EB #105, Vertiport Design. FAA vertiport guidance is updated over time to address the variety of aircraft and operations seeking EIS.

Airport sponsors or proponents submit a Form 7460-1, Notice of Proposed Construction or Alteration, in accordance with 14 CFR § 77.9 for any proposed onairport (or on-heliport) vertiport support infrastructure (e.g., charging stations, fueling stations, AAM terminal). Airport sponsors with federally obligated facilities, which are airport sponsors who have accepted federal financial assistance, must also conduct proper planning activities including an update to their FAA-approved Airport Layout Plan.

Sponsors of non-federally obligated facilities or proponents of a new vertiport facility not on or co-located with an existing federally obligated airport or heliport submit a Form 7480-1, Notice of Landing Area Proposal, at least 90 days in advance of the day that construction work is to begin on the landing area. This notification to the FAA is required in accordance with 14 CFR part 157, Notice of Construction, Alteration, Activation, and Deactivation of Airports.

New vertiport facilities that require approval and/or funding from FAA will undergo FAA environmental review. Facilities that do not require FAA approval or funding may be expected to engage in community engagement consistent with any applicable local rules.

All non-FAA stakeholders will have agreed to established criteria for ground infrastructure, including: vertiport location, charging, cooling, maintenance, security, ground safety, and parking in accordance with federal regulations where applicable. Take-off and landing from the Touchdown and Liftoff Area (TLOF) is recommended for approach and departure operations from a standalone vertiport or vertistop (vertiport with limited services). It is unlikely that AAM operators will use “hover taxi” to taxi or re-position on the airfield due to anticipated battery limitations.

## Security

Security is a key component to the safe and secure integration of AAM. However, AAM presents unique challenges for aviation security. Therefore, a Working Group under the broader DOT-lead Interagency Working Group previously discussed was established to focus strictly on security issues to inform the whole of government strategy for addressing the integration and evolution of AAM as required in the AAM Coordination and Leadership Act.

## 4.3 I28 Scenario

The following provides a glimpse of what I28 might look like once an AAM aircraft has successfully completed the certification processes (including wake turbulence classification)2 and is ready to fly. This scenario sequence reflects the use of designated operating areas, to include landing and departure areas, other existing infrastructure, services, and existing policies and procedures to the degree possible. LOA negotiations between air traffic, OEMs and operators, airport operators, port authorities, emergency management services, and federal, tribal, state, and local law enforcement organizations establish the processes and procedures for safe and efficient operations.

This simplified thread steps through an I28 AAM operation departing a vertiport in uncontrolled airspace and landing at a tower-controlled airport in controlled airspace:

1. The pilot follows established procedures for checking weather and NOTAMs for departure, en route, and destination, and files a flight plan if required. While passengers prepare to board the AAM aircraft, the pilot conducts aircraft walkarounds, preparations, safety protocols, and departure checklists.

2. Departing in uncontrolled airspace, the pilot is responsible for adhering to appropriate rules governing flight in uncontrolled airspace. The pilot announces their departure intentions over a common radio frequency and maneuvers the aircraft to the takeoff location. After visually ensuring their departure area and path is clear, the pilot departs.

3. The pilot is aware of the requirements for flight in controlled airspace. The aircraft enters controlled airspace by means of two-way radio communication and the appropriate clearance from ATC. Published procedures or agreements (national, local, or signatory) reduce the need for ATC communications.

4. ATC issues instructions or clearances to provide separation and/or sequence the aircraft with other traffic. The pilot on board complies with instructions given by ATC or follows previously coordinated and approved instructions from the approving ATC facility (via published procedures or agreements).

5. ATC transfers control and communication from controller to controller as the aircraft transits different ATC sectors. After the pilot obtains information on destination runway(s) in use, weather, and other pertinent airport information, they start their approach to the landing site or follow a previously approved approach path. The ATC tower issues a clearance to land. The pilot may ask and be permitted to land at airport areas other than runways and taxiways.

6. The pilot on board completes landing checklists, their approach, and safe landing at a new, existing, or predetermined approved landing site. The aircraft is maneuvered to the approved parking area for deplaning.

7. Passengers and crew follow established procedures for deplaning the aircraft. Following prescribed security procedures, the passengers exit the area or are directed to any further security screening required to enter the secure terminal area for connecting flights.

This is a high-level view of I28 operations and the near-term integration phase. The assumptions, expectations, and nature of operations will evolve over time to reflect the technology and infrastructure advancements that will provide increased scalability and types of operations.

## 5 Innovate28 Workstreams

The FAA is taking a holistic approach to the efforts required for AAM implementation. The I28 leadership team in the NextGen organization (ANG) established iTeams comprised of representatives across FAA lines of business (LOBs) to bring together expertise in different areas associated with AAM implementation and foster collaboration in the planning and execution of required activities. The iTeams represent the major workstreams associated with AAM implementation, including Certification, Airspace and Air Traffic Management, Infrastructure, Environment, Hazardous Materials Safety, and Community Engagement.

This section addresses each workstream and describes the activities completed or underway, as well as gaps to be addressed, to support near-term I28 implementation goals. Integrating this information supports the development of a coordinated roadmap to I28 AAM operations. While the initial focus is on enabling near-term AAM operations, the work efforts and milestones within these workstreams will continue beyond I28 to support the continuous evolution of AAM.

## 5.1 Certification

The FAA has a proven track record of safely certificating and integrating new and novel design features, aircraft, and safety-enhancing technologies into the NAS. New AAM aircraft are expected to offer capabilities ranging from single-pilot, recreational eVTOL aircraft, to piloted, powered lift, multi passenger short range aircraft. The type certification of AAM aircraft is possible because the FAA can leverage the current regulatory framework, which allows development of project-specific requirements tailored to

![9d96b7035fa63421c67e275e5f3854cf39ed8dfd70b62953c0e896a2b5653edc.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/9d96b7035fa63421c67e275e5f3854cf39ed8dfd70b62953c0e896a2b5653edc.jpg)

fit the unique aspects of novel designs. The flexibility to tailor requirements can come in the form of special conditions or unique airworthiness criteria under a special class, depending on the AAM design (airplane, rotorcraft, or powered lift).

## 5.2 Operational Suitability

As AAM aircraft near issuance of their Type Certificate, the OEM will engage with multiple boards within the FAA’s Flight Standards Service (AFX) to conduct operational suitability reviews. It is during this process that the Flight Standardization Board will determine the aircraft type rating, the Maintenance Review Board will determine the scheduled maintenance taskings for development of an operator maintenance program, and the Flight Operations Evaluation Board will determine the requirements of the aircraft’s master minimum equipment listing. The applicant may also apply for any needed regulatory exemptions during this process.

## 5.2.1 Operations Certification

To satisfy regulatory responsibilities and promote convergence, AAM industry engagement concerning operations certification will resemble a mix of traditional aviation with one-on-one engagement combined with utilization of existing and/or new forums that invite FAA-industry (e.g., standards development organizations) collaboration. In other words, the FAA will use normal processes with a mix of

![5551af178aaa00471b9f7ba80c4a8524b7dcf84b71b90f1fb7a50f9822a00647.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/5551af178aaa00471b9f7ba80c4a8524b7dcf84b71b90f1fb7a50f9822a00647.jpg)

one-on-one outreach with individual applicants, and larger groups via forums to achieve a successful collaboration. This is a key procedural step in setting common expectations across the industry.

The FAA is engaged in rulemaking to enable AAM operations. The efforts are currently oriented around piloted operations, and in the interim the agency expects to use waivers, deviations, and exemptions as appropriate for initial operations. For AAM operations to be successful in 2028, it is important to connect, as seamlessly as possible, the interim methods with proposed rulemaking (and an overall framework, including external and internal guidance) as operational experience accrues.

## Rulemaking Activities

Integration of Powered Lift: Pilot Certification and Operations: Publication of a Notice of Proposed Rulemaking (NPRM) is expected in June 2023. This action proposes an SFAR for alternate eligibility requirements to safely certificate initial groups of powered lift pilots, as well as determine which operating rules to apply to powered lift aircraft on a temporary basis to enable the FAA to gather additional information and determine the most appropriate permanent rulemaking path for these aircraft.

Recognition of Pilot in Command Experience in the Military and Air Carrier Operations: The final rule was published on September 21, 2022. This action extended the 500-hour credit military pilots of fixed-wing airplanes can use towards the 1,000 hours of air carrier experience to pilots of powered lift aircraft operations. This allows credit for select military time in a powered lift aircraft flown in horizontal flight towards the 250 hours of airplane time as pilot in command (PIC), or second in command performing the duties of PIC, required for an airline transport pilot certificate.

Update to Air Carrier Definitions: This NPRM was published on December 7, 2022, with comments submitted by February 6, 2023. This action proposes to amend the regulatory definitions of certain air carrier and commercial operations. The proposed rule adds powered lift to these definitions to ensure the appropriate sets of rules apply to air carriers' and certain commercial operators' operations of aircraft that FAA regulations define as powered lift. The FAA also proposes to update certain basic requirements that apply to air carrier oversight, such as the contents of operations specifications and the qualifications applicable to certain management personnel. In addition, this action proposes to apply the rules for commercial air tours to powered lift. This proposed rule is an important step in the FAA's integration of this new entrant aircraft in the NAS.

Airman Certification Standards and Practical Test Standards for Airmen; Incorporation by Reference: This NPRM was published on December 12, 2022, with comments submitted by February 10, 2023. This action proposes to revise certain regulations governing airman certification. Specifically, the FAA Airman Certification Standards and Practical Test Standards are currently utilized as the testing standard for practical tests and proficiency checks for persons seeking or holding an airman certificate or rating. The FAA proposes to incorporate these Airman Certification Standards and Practical Test Standards by reference into the certification requirements for pilots, flight instructors, flight engineers, aircraft dispatchers, and parachute riggers.

The following list includes examples of guidance that may need to be developed or updated in support of AAM integration rulemaking activities to describe standards and means of compliance, as well as promote good safety practices. This list is not all-inclusive.

Advisory Circulars

Development of standards and practices for Flight Standardization Boards and Maintenance Review Boards

• Processes and Procedures for issuance of 14 CFR part 135 Air Operator Certificates

• Amendment of internal FAA Orders and related change management

• FAA Order 8900.1 Flight Standards Information Management System

FAA Order 8260-series

• Development of training for workforce to support AAM oversight and certification

Development of and guidance related to the issuance of Operations Specifications (OpSpecs), Management Specifications (MSpecs), Training Specifications (TSpecs), and Letters of Authorization as appropriate, for AAM Operations

• Guidance and procedures for the issuance of licensing and certification of industry personnel

• Aeronautical Information Manual (AIM) and Aeronautical Information Publication (AIP)

Pilots Handbook of Aeronautical Knowledge

Flight Standards infrastructure guidance

Flight Standards is working to further adapt its organizational structure for both conventional and emerging operations. Aircraft capabilities and procedures (defined by manufacturers) are inextricably linked with operational approvals and personnel training, along with procedures for flight operations and continued airworthiness. As such, Flight Standards will continue to work closely with the FAA’s Aircraft Certification Service (AIR) as part of an integrated oversight strategy by dovetailing its efforts with the certification of AAM aircraft and the issuance of Type Certificates (and continuous operational safety after entry into service).

Flight Standards is evolving its tools used for coordination of manufacturer/operator applications to increase efficiencies and enhance communications. For simple certifications, some steps can be condensed or eliminated. Some applicants may lack a basic understanding of what is required for certification. Other applicants may propose a complex operation but are well prepared and knowledgeable. Because of the variety in proposed operations and differences in applicant knowledge, processes will be thorough and flexible enough to apply to all possibilities. Industry applicants have the responsibility for compliance. Flight Standards will ensure applicants are aware of applicable regulations, standards, and requirements.

Flight Standards is making improvements to the prioritization and processing of certification of new operators and repair stations. This includes exploring various ways to reduce wait times, while ensuring resources available to support valid business ventures. Similarly, as with conventional aviation and drone operations, surveillance and oversight will be scaled taking a risk-based approach, ensuring application of the right level of FAA (and industry) resources. For cases where direct oversight is not applied as frequently, the FAA will work with industry on broad safety promotion and compliance activities.

## 5.2.2 Aircraft Certification

Aircraft certification is a process through which the FAA approves the design, production, and airworthiness of aircraft in the U.S. The certification process ensures that an aircraft meets minimum safety and environmental standards set by the FAA before it can be operated commercially or privately in the U.S. airspace.

The certification process involves several stages, including design approval, production approval, and airworthiness approval. Design approval involves reviewing and approving an aircraft's proposed design, including its systems, structures, and performance capabilities. Production approval ensures that an aircraft is built according to the approved design and meets the FAA's quality standards. Finally, airworthiness certification ensures that the aircraft is in a condition for safe operation and conforms to its approved design.

Currently, AIR is engaged with over two dozen manufacturers targeting the development of novel aircraft and propulsion technologies that underlie the design and operation of AAM aircraft. While some of these companies are relatively early in their technology development, vehicle design, and operations concepts, and in their readiness to engage in a new type certification program, nearly half of the companies have reached a level of maturity and development to have manufactured flying testbed prototypes. Their progress reflects positively on readiness to advance in the type certification process.

AIR is also currently working to define clear certification requirements and pathways to showing compliance for several novel aircraft technologies that are anticipated to be key to the future of AAM design and operations. These technologies include electric propulsion, large lithium-ion battery arrays, hydrogen fuel cell systems for electrical energy supply, distributed propulsion systems with highly integrated flight and propulsion controls, increased automation, and VTOL capabilities for winged aircraft.

The FAA determined that its existing aircraft certification processes are sufficient to type certificate powered lift as a special class under 14 CFR § 21.17(b). The special class process allows the FAA to address the novel features of unique and nonconventional aircraft without the need for additional processes such as special conditions or exemptions that would be required if the FAA used existing airworthiness standards. Under the special class process, the FAA designates or creates applicable airworthiness requirements as the certification basis for each aircraft design, including its engines and propellers. This designation and creation of applicable airworthiness requirements includes appropriate requirements from the existing airworthiness standards applicable to normal category and transport category airplanes, normal category and transport category rotorcraft, aircraft engines and propellers (parts 23, 25, 27, 29, 33, and 35), and it may also include unique airworthiness criteria developed specifically for the individual product.

In order to move forward to a more streamlined certification process, the FAA has proposed an update and expansion of the requirements for Safety Management Systems (SMS) and requires 14 CFR parts 5, Safety Management Systems, 21, Certification Procedures for Products and Articles, 119, Certification: Air Carriers and Commercial Operators, 91, and 135 certificate holders to develop and implement an SMS. The FAA also proposed this rule in part to address a Congressional mandate as well as recommendations from the National Transportation Safety Board (NTSB) and two Aviation Rulemaking Committees (ARCs). The Notice of Proposed Rulemaking on Safety Management Systems was published in the Federal Register on January 11, 2023, and the comment period closed on April 11, 2023.

## Acceptable Means of Compliance

A key tenet of the FAA’s approach to AAM certification is that an applicant’s means of demonstrating compliance with the airworthiness requirements for its proposed design (i.e., the applicant’s Means of Compliance (MOC)) must be accepted by the FAA. Although the FAA is leveraging the performance-based requirements from 14 CFR part 23 as modified by amendment 23-64, the consensus standards that the FAA has accepted as MOCs for normal category airplanes may not be appropriate for a particular proposed AAM due to its configuration, complexity, or novel technology. Work is still in progress to provide applicants with standardized MOCs that consider configuration differences, complexity, and novel design.

## Noise Considerations

Aviation noise remains one of the primary environmental challenges to the continued growth of aviation. Pursuant to 49 U.S. Code (U.S.C.) 44715, the FAA has the responsibility to “protect the public health and welfare from aircraft noise.” This responsibility includes broad authority to adopt regulations and noise standards as necessary. The FAA regulates the maximum noise level that an individual civil aircraft can emit through requiring aircraft to comply with certain noise limits. These limits and associated testing standards are found in 14 CFR part 36, Noise Standards: Aircraft Type and Airworthiness Certification. Any applicant seeking a type certificate for their aircraft in the U.S. must comply with noise standard requirements as a part of the type certification process.3 In addition, the FAA must complete a Noise Control Act finding, which ensures that the latest safe and airworthy noise reduction technology is incorporated into aircraft design and enables the reductions in noise experienced by communities.

When establishing the noise certification basis for AAM, the FAA will examine each application and determine whether existing part 36 requirements are appropriate as a noise certification basis, as is done for all applicants whose aircraft are subject to noise certification. If the current standards cannot be appropriately applied, the FAA may promulgate a rule of particular applicability for that applicant’s aircraft model to establish a noise certification basis. Such a rule will require environmental review pursuant to the National Environmental Policy Act (NEPA). To date, for the one aircraft presented for noise certification, the FAA has determined that the existing testing procedures and requirements in part 36 are applicable. The FAA is currently evaluating other applications and will determine the noise certification basis for them.

## 5.3 Airspace and Air Traffic Management

AAM infrastructure, automation, and traffic management approaches will evolve over time as the AAM operational tempo increases in airspace across the NAS. AAM aircraft will be integrated at greater scale with commercial and general aviation (GA) traffic, as well as other low-altitude airspace users, such as recreational and commercial small unmanned aircraft systems or drones. In the near-term for I28, however, these interactions are minimized and thus can be managed with existing ATC tools, procedures, and protocols. AAM aircraft are expected to be operating with a pilot on board and under VFR in VMC conditions; it is likely these aircraft will be treated as any other fixed wing/rotorcraft operating under VFR conditions, to the extent they are able to comply with existing rules, regulations, and procedures.

![acc2ff982eade759be3098ed52d93034129e86288ece30ce4343ace60bfe0687.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/acc2ff982eade759be3098ed52d93034129e86288ece30ce4343ace60bfe0687.jpg)

The FAA’s Air Traffic Organization (ATO) leads the planning, development, and implementation of airspace and ATM solutions, including development of airspace and route structures, policies, procedures, and ATC training. For I28, the ATO developed a general approach for airspace route design and usage, and traffic management that supports AAM VFR operations in the near-term (see Section 4), including the use of existing VFR route constructs.

I28 ATM processes will support a future national strategy, and supplemental directives will ensure consistency in how AAM route networks are designed. Existing mechanisms used by air traffic beyond traditional airspace classifications include the establishment of a special air traffic rule which applies within a Special Flight Rules Area (SFRA). Evaluation of these and alternative methods early in the planning process will allow the required collaboration to ensure timely resolution and publication of AAM route and network design.

Depending on the volume and specific operational needs of I28 operations, local air traffic facilities may need to update their procedures, utilize existing non-rulemaking airspace strategies, and complete an analysis to determine the need for airspace changes. The air traffic planning and analysis policy uses an interdisciplinary approach to effectively manage NAS changes. This would include the development of necessary training in a training delivery plan.

Sufficient time will be allotted throughout I28 development activities to ensure the necessary rulemaking or non-rulemaking activities, route publications and distribution, and training materials can be developed; and controller training can be completed to support the safe management of NAS operations.

In parallel, the ATO will continue to address AAM through its ATO AAM Near-Term Operational Integration Workgroup (NTIWG), which was established in November 2021 to identify air traffic considerations and impacts for near-term operations. After concluding their review in June 2022, the NTIWG had identified 55 recommendations to help address the integration of AAM operations in the near-term. Many of the recommendations require changes to FAA policy and guidance directives including, but not be limited to:

JO 7110.65 Air Traffic Control

• JO 7210.3 Facility Operation and Administration

• JO 7400.2 Procedures for Handling Airspace Matters

The ATO also recommends a detailed policy review be conducted to determine if other associated orders and ACs need to be updated or developed. Topics that should be considered include:

Wake Turbulence Categorization and impacts to operations

• Aircraft Certification and how that translates to ATC Service Provisions and Separation

Minimum Safe Altitude as it applies to AAM

Workforce and facility staffing considerations

## 5.4 Infrastructure

AAM operations require specialized infrastructure to support the safe and efficient operation of eVTOL aircraft. This section addresses how existing infrastructure can be leveraged to support near-term operations. It also documents what has been completed to-date to enable the planning, design, and construction of new vertiports or modification of existing facilities. The FAA remains committed to fostering collaboration with industry and local stakeholders to enable vertiport construction. Additional aspects of infrastructure will need to be addressed as I28 efforts progress, including electrification to support charging of AAM aircraft and power for AAM operations. The DOT Interagency Working Group will address these and other topics not directly in the FAA’s purview.

## 5.4.1 Existing Infrastructure

To enable near-term operations, operators and manufacturers desire to use existing infrastructure, including commercial service airports, underutilized GA airports, and heliports. It is likely though that existing heliports and airports will require modification or enhancements to accommodate early entry aircraft and their unique operations.

Facility owners and operators should plan for dedicated takeoff and landing areas and support facilities that address the needs of eVTOL operators, including limited taxi capabilities and charging. Airport and heliport owners should engage existing and future tenants who intend to operate eVTOL aircraft to ensure planning and siting of infrastructure and equipment adequately accommodates their intended operations.

Construction of on-airport vertiport facilities may require FAA notification under 14 CFR part 77, Safety, Efficient Use, and Preservation of Navigable Airspace and updates to an airport’s FAA approved Airport Layout Plan (for federally obligated airports). Modifications to existing federally obligated infrastructure will also undergo FAA environmental review and community engagement. Facilities that do not require FAA approval or funding may be responsible for community engagement consistent with local rules.

## 5.4.2 New Infrastructure

Communities, developers, and operators may also choose to establish new vertiports, not co-located with an existing airport or heliport. State licensing and local zoning ordinances may require updates to accommodate these new types of landing facilities. Where no federal funding is used, FAA oversight and engagement with these new vertiports and their surrounding communities may be limited. Communities are encouraged to plan for vertiports capable of accommodating multiple operators that will benefit passengers. They should also plan for equitable, multimodal placement of vertiports to connect transportation systems without creating new sources of traffic congestion and parking concerns whenever possible. Construction of new infrastructure would trigger FAA notification under 14 CFR part 157.

## 5.4.3 Vertiport-Related Research

In 2019, the Office of Airports (ARP) and the Airport Technology Research and Development Branch (ATR) began a multi-year research project to support the development of vertiport standards. ATR is investigating and evaluating VTOL and STOL aircraft design and performance to develop design standards and guidance.

For Phase 1, ATR completed a literature review (2021) that identified gaps in available performance data; a result of AAM company concerns about the release of proprietary information. With the help of FAA’s Emerging Technology Coordination Branch (formerly known as Center for Emerging Concepts and Innovation) and other AIR offices, using existing mechanisms for communication with applicants and data protection, ATR obtained preliminary AAM aircraft data. The literature review findings, analysis of the aircraft data, and further interchange with manufacturers and operators, supported the development of interim guidance. On September 26, 2022, ARP released EB #105, Vertiport Design. The EB serves as interim guidance to airport sponsors, vertiport operators, and infrastructure developers for the design of vertiports for VTOL operations, until a performance-based AC is released in 2025. The EB is prescriptive and purposely limited to address eVTOL operations using design and performance data available from VTOL aircraft manufacturers currently working toward certification.

Phase 2 of the research was completed in summer 2022 and involved six hypothetical vertiport locations covering a range of diverse scenarios, including on-airport, off-airport (in close proximity to complex airport environment), urban, and rural vertiport environments. Modeling analyzed TLOF occupancy times for arrival and departure operations. The scenarios used site-specific information, allowing development of conceptual layouts for each scenario in an airport layout plan-style drawing.

Phase 3 of the research (started in January 2023) included simulation exercises and operation testing with various AAM companies. The simulation exercises will support preparations for on-site operational testing which will further evaluate landing precision, approach/departure profiles, rotorwash/downwash impacts, and aircraft taxiing.

The FAA also has an interagency agreement with the Department of Energy’s National Renewable Energy Lab (NREL) to determine how aircraft electrification affects a vertiport, heliport, or airport’s electrical grid. The research will look at vertiport charging requirements, hazards associated with charging stations, and cybersecurity.

Collaboration among FAA organizations and research branches has been key to ensuring FAA research is relevant and addresses the variety of operations anticipated for I28 and beyond. ARP receives notification of new and innovative aircraft and technology through the AIR Intake Board and other collaborative processes, and then facilitates introductions, as needed, between AIR, the manufacturer, and ATR. The FAA iTeams will continue to coordinate and collaborate on research areas of overlap.

To enable near-term operations, the following areas require further research:

• Vertiport fire extinguishment equipment and electric aircraft firefighting tactics

• VTOL aircraft parking needs

• Vertiport signage, markings, and lighting

## 5.4.4 Vertiport Standards and Oversight

The FAA is using existing policy, regulations, and infrastructure as a baseline for vertiport guidance and regulations development; however, it will be the responsibility of the operators, manufacturers, state and local governments, and other stakeholders to plan, develop, and enable vertiport infrastructure for I28 operations.

The FAA cancelled its AC on Vertiport Design in 2010 due to a lack of commercially available aircraft. Standards are needed to address the wide variety of aircraft and operations intended under AAM. While the FAA published prescriptive interim guidance for the design of vertiports in EB #105 in September 2022, ARP plans to release a performance-based AC in 2025. Data obtained through operational testing of prototype and production VTOL and STOL aircraft will greatly influence design standards and guidance in the AC. Since AAM is constantly evolving, ARP anticipates updating the vertiport AC more frequently than other airport-related ACs.

The FAA also established a cross-LOB/staff office ‘Vertiport Process Improvement Team’ to identify a path forward with developing criteria and standards for processing and analyzing proposed vertiports. This team identified actions necessary to address gaps in existing policies, procedures, and standards, including but not limited to the following:

Initiate a rulemaking project for 14 CFR parts 77, Safe, Efficient Use, and Preservation of the Navigable Airspace, and 157 to clarify applicability to vertiports and supporting infrastructure and define vertiport imaginary surfaces

Review and update JO 7400.2 Airport Airspace Chapter to address vertiport infrastructure and imaginary surfaces

Review and update FAA Forms 7460-1 and 7480-1 to identify and address vertiport/supporting infrastructure information and data needed for FAA processing/review

Define FAA’s role in vertiport inspections

Existing statutory authority may limit the agency’s ability to regulate (i.e., 14 CFR part 139, Certification of Airports) and fund vertiports, particularly for private-use facilities. Without certification or federal funding, facilities may not comply with FAA design standards (a current condition that exists in many heliports) or have similar safety equipment and firefighting equipment onsite like today’s commercial service airports.

## 5.5 Environment

The FAA is responsible for evaluating the significance of environmental impacts for aviation operations in the U.S. and disclosing those impacts to the public. As such, to enable nearterm AAM operations, the FAA will consider the impact of AAM aircraft on a variety of aspects of the human environment, including (but not limited to) noise, air quality, visual disturbances, and disruption to wildlife. The FAA has policies and practices in place to conduct environmental review for legacy aviation. However, the FAA is still evaluating how best to streamline the environmental review process for new entrants, such as AAM.

![bd67f879035d1cdd22000d4873921a00a5b4eb94c556b0286e14f62c24927387.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/bd67f879035d1cdd22000d4873921a00a5b4eb94c556b0286e14f62c24927387.jpg)

The majority of questions related to compliance with environmental requirements in support of I28 remain open due to the need for additional information on what FAA approvals will be required for different aspects of the operation and any infrastructure, and what FAA offices will be responsible for such approvals. In addition, further information from manufacturers and operational data for aircraft is needed for the analysis of noise and emissions impacts. In particular, in order to determine whether compliance with NEPA is required, the FAA will need to identify whether there is/are a major federal action(s) triggering NEPA. Certification of aircraft, such as AAM, is a major federal action that will trigger compliance with NEPA, however there may be other FAA actions (e.g., approving or establishing where the AAM aircraft fly) that could trigger NEPA. For example, developing routes for AAM aircraft or introducing AAM into the NAS that will impact other flight operations may trigger NEPA. If NEPA applies, the LOB responsible for the approval will need to determine and conduct the appropriate level of environmental review (including potentially public involvement), as well as consider the need for supplementary community engagement.4

The FAA’s Office of Environment and Energy (AEE) and the Office of the Chief Counsel (AGC) will provide support and advice to FAA LOBs in identifying applicable actions and determining the appropriate level of environmental review and associated public involvement and community engagement. If environmental reviews are required, the applicable LOB(s) will be responsible for planning, coordinating, and (where applicable) funding the environmental review and provide any associated public involvement and community engagement needed.

## 5.6 Hazardous Materials Safety

As AAM operations are initially expected to be conducted under 14 CFR part 135, AAM operators will be required to have hazardous materials training programs approved by the FAA; hazardous materials manuals accepted by the FAA; and Operations Specifications permitting or prohibiting accepting, handling, and transporting HazMat. These requirements apply whether or not a part 135 certificate holder chooses to transport hazardous materials. Part 135 HazMat training and manual requirements are functionbased and scale to the scope and complexity of a certificate holder’s operation.

DOT Hazardous Materials Regulations (HMR; 49 CFR parts 171-185) apply to any operator transporting hazardous materials in commerce. The HMR are promulgated by the Pipeline and Hazardous Materials Safety Administration (PHMSA). Regulations applicable to aviation are promulgated in coordination with the FAA.

As part of an operator’s SMS, safety risk assessments accounting for hazardous materials being transported, relative to a specific certificate holder’s system, can help to inform supplemental risk management strategies in AAM operations.

## 5.7 Community Engagement

Changes in airport operations, airspace procedures, aviation infrastructure, and technology can have effects on communities. When developing a new project or procedure that may impact the public, the FAA proactively engages with airports, communities, and elected officials to better understand community concerns about aviation noise and in some cases adjust or mitigate these concerns. With AAM, the FAA will proactively engage with airports and elected officials to ensure they understand AAM and expected operations. Currently the scope of what may need to change to accommodate the safe integration and operation of AAM operators into the airspace is evolving. The FAA’s level of engagement will follow the level of change; however, given the expected scope of AAM changes, the FAA does not expect the same type of engagement that the agency conducts for major airspace changes.

Engagement at the regional level is the most effective path as AAM stakeholders and the FAA consider key site locations for I28. The FAA’s Community Involvement Manual provides flexible guidance and best practices applicable to all FAA actions and will be leveraged for AAM operations and I28. Additional guidance also exists specifically related to airspace procedures. While the FAA does not expect to develop new or unique agency policy, it will be important to ensure all aspects of the I28 project utilize these best practices.

Elements of community engagement are already part of normal business practices for some FAA LOBs or Staff Offices. For example, compliance with NEPA and other environmental requirements often includes required public involvement elements, such as the distribution of an environmental document for public review and comment, that might be one element of a robust community engagement strategy. It is important to note that community engagement supplements but cannot substitute for these required public involvement activities. While public involvement is led by the FAA under some environmental laws or other requirements, community engagement may also be led by the proponent of the project (which may be FAA in the case of many airspace changes but can also be airport sponsors or operators). When the project proponent takes the lead on community engagement, the FAA plays an oversight role, providing advice and guidance on good community engagement practices.

For I28, community engagement needs to focus on more than just airspace and it will involve DOT/FAA and other agency offices. It is important that the public understand how these new aircraft operations will impact their communities. Many other stakeholders, such as AAM operators, vertiport sponsors, and airport operators, will be part of bringing AAM to an operational reality and will have a role in community engagement.

## 6 Innovate28 Integrated Schedule

The Integrated Master Schedule (IMS) contains a comprehensive list of activities that must be achieved by FAA LOBs and staff offices, industry, and local governments and stakeholders to enable AAM operations at a key site. The IMS is generic for a key site and will be tailored for each individual implementation, including the I28 building blocks, as more information is available. Not all activities included in the comprehensive generic IMS will be required for every implementation, and individual implementations will require additional site-specific activities. As a result, the IMS will be iterative as the team learns from each implementation. The IMS utilizes dependencies between activities which are included in Table 1. The IMS requires further refinement both within the agency and through collaboration with external stakeholders, including industry.

## The following lists some considerations for the IMS as displayed in Figure 1:

The Type Certification and Operational Certification paths shown in the IMS are examples for a typical OEM/operator. The certification timelines can vary significantly depending on the maturity and responsiveness of the OEM/operator. Some OEMs have already completed part(s) of the certification processes shown here.

The Environmental Review timeline is based off a typical Environmental Assessment. This timeline can range significantly based on site-specific factors that can either reduce the Environmental Review to a Categorical Exclusion when the proposed federal action does not individually or cumulatively have a significant effect on the human environment and the proposed action falls within the scope of the approved agency categorical exclusions; or increase it to an Environmental Impact Statement which is required under NEPA when a proposed federal action significantly affects the human environment.

The timelines of some activities could potentially be significantly reduced or eliminated if it is determined that existing infrastructure can be leveraged with little to no modification.

The final state of the IMS will list a duration and point of contact for each activity so its status can be tracked at routine check-in meetings.

Figure 1. Integrated Master Schedule Version 1.0  
![076886697e5e522b737fd5f2410126fd0359885eb14f3b9585a6df3e555989c8.jpg](https://aam-wiki.gksj.cc/uploads/images/gallery/2026-05/scaled-1680-/076886697e5e522b737fd5f2410126fd0359885eb14f3b9585a6df3e555989c8.jpg)  
Note : The IMS is a depiction of the activities that may be required to allow an operator to enter into service at a location. Depending on the scope and concept of use for their planned operation, not all activities may be required for every implementation; the duration of a step may vary by project as well. Some companies have already completed some of these activities.

Table 1. Detailed List of Activities in the Integrated Master Schedule Version 1.0
<table><tr><td rowspan=1 colspan=2>High-level Activity</td><td rowspan=1 colspan=3>Sub-activities</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=1>High-level Activity</td><td rowspan=1 colspan=1>Sub-activities</td></tr><tr><td rowspan=1 colspan=2>Select Site</td><td rowspan=1 colspan=3>Local discussions and buy-in</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Operational Certification</td></tr><tr><td rowspan=1 colspan=2>National VertiportActivities</td><td rowspan=1 colspan=3>Vertiporteratinalestiatcollection and analysis</td><td rowspan=8 colspan=2></td><td rowspan=1 colspan=1></td><td rowspan=8 colspan=1>Operational Suitability</td></tr><tr><td rowspan=2 colspan=2>Vertiport AC</td><td rowspan=2 colspan=3>Vertiport ACRulemaking project fa157</td><td></td><td rowspan=1 colspan=1>Maintenance ReviewBoard (MRB) andReport (MRBR)</td></tr><tr><td></td><td rowspan=2 colspan=1>CodtiBoard(FOEB)</td></tr><tr><td rowspan=3 colspan=2>State VertiportActivities</td><td rowspan=1 colspan=3>Update zoning ordinances</td><td></td></tr><tr><td rowspan=1 colspan=3>Update icensing requirements toaddress vertiports</td><td></td><td rowspan=1 colspan=1>Issue Master Minimum EquipmentListing (MMEL)</td></tr><tr><td rowspan=1 colspan=3>State environmentalpolicy review</td><td></td><td rowspan=1 colspan=1>Revifor Continued Airworthiness(CA&#x27;s)</td></tr><tr><td rowspan=7 colspan=2>Local On-Airport/FederallyFunded VertiportActivities</td><td rowspan=1 colspan=3>Airport plannin actities</td><td></td><td rowspan=2 colspan=1>ReviewandCocur ita FManuals nd Fight ManualSupplements</td></tr><tr><td rowspan=2 colspan=3>Airport Layout Plan (ALP)development, submission, andapproval process</td><td rowspan=1 colspan=2></td><td></td></tr><tr><td rowspan=4 colspan=2></td><td rowspan=5 colspan=1>Operational Approval(Part 135)</td><td rowspan=1 colspan=1>Phase 1: Pre-application</td></tr><tr><td rowspan=4 colspan=3>Section 163 reviewNEPA Environmental ReviewSite Engineering7460 processReceie statelicensin</td><td rowspan=1 colspan=1>Phase 2: Formal Application</td></tr><tr><td rowspan=1 colspan=1>Phase 3: Design Assessment</td></tr><tr><td rowspan=1 colspan=1>Phase 4: Performance Assessment</td></tr><tr><td rowspan=1 colspan=2></td><td rowspan=1 colspan=1>Phase5:Administative Function</td></tr><tr><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>ConstructionPublication and charting</td><td rowspan=4 colspan=2></td><td rowspan=4 colspan=1>Review and Update AirTraffic Policy</td><td rowspan=1 colspan=1>7110.65 Document Change Proposal(DCP)</td></tr><tr><td rowspan=3 colspan=2>Local Off-Airportinon-Federally FundedVertiport Activities</td><td rowspan=1 colspan=3>7480 processReceie statelicensin</td><td rowspan=1 colspan=1>Revieandate40.Airspace Chapter</td></tr><tr><td rowspan=2 colspan=3>Design and Construction</td><td rowspan=2 colspan=2></td><td></td></tr><tr><td rowspan=1 colspan=1>Reviewand update FAA Foms7460-1and 7480-1</td></tr><tr><td rowspan=1 colspan=2></td><td rowspan=1 colspan=3>Type Certification</td><td></td><td></td><td rowspan=1 colspan=1>Spectrum Analysis</td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=6 colspan=2>Conceptual Design</td><td rowspan=6 colspan=3>Process OrientationPre-Project GuidanceFamiliaization riefing</td><td rowspan=3 colspan=2></td><td rowspan=3 colspan=1>Controller Training</td><td rowspan=1 colspan=1>Develop training plan</td></tr><tr><td rowspan=3 colspan=2></td><td></td></tr><tr><td rowspan=1 colspan=1>Schedulecontrollr rainingTrain controllers</td></tr><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Develop and Ilmplement Air Trfi Procedure(s)</td></tr><tr><td></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Phase 1: Scoping</td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=2 colspan=2></td><td rowspan=3 colspan=1>Phase 2: ProcedureSolution Development (6months or more)</td><td rowspan=3 colspan=1>nitialdesiactiviteefinemnt,validation</td></tr><tr><td rowspan=1 colspan=2>Application</td><td rowspan=2 colspan=3>Aplication for TC and PCEstablishment of TC ProjectCetifictionPret Nic</td></tr><tr><td rowspan=1 colspan=2>Requirements</td><td rowspan=1 colspan=1></td><td></td></tr><tr><td rowspan=2 colspan=2>Definition</td><td rowspan=2 colspan=3>Form the Crtiction Team</td><td></td><td></td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Initial Environmental look</td></tr><tr><td></td><td rowspan=2 colspan=1></td><td rowspan=2 colspan=1>Phase 3: Evaluation 12-18months)</td><td rowspan=1 colspan=1>SMS/SRM Panel and Process</td></tr><tr><td rowspan=2 colspan=2></td><td rowspan=1 colspan=3>The Preliminary TCB eeting</td><td></td><td rowspan=1 colspan=1>Environmental Review</td></tr><tr><td rowspan=1 colspan=1></td><td rowspan=1 colspan=3>Issue Paper ldentification</td><td></td><td rowspan=2 colspan=1></td><td rowspan=2 colspan=1>Phase 4: Implementation</td><td rowspan=1 colspan=1>Finalize SOP and LOA</td></tr><tr><td rowspan=4 colspan=2>Certification Basisand DDsRequirements&#x27;Definition</td><td rowspan=1 colspan=1>sis</td><td rowspan=1 colspan=3>G-1 Cetifiction Basis</td><td rowspan=1 colspan=1></td><td rowspan=1 colspan=1>Procedure processing and publication,including fliht inpection</td></tr><tr><td rowspan=2 colspan=3>Notice of proposed airworthinesscriteria</td><td rowspan=1 colspan=1></td><td rowspan=2 colspan=1></td><td rowspan=2 colspan=1></td><td rowspan=1 colspan=1>Charting</td></tr><tr><td rowspan=1 colspan=2></td><td rowspan=1 colspan=1>Aircraf ype auomationupe</td></tr><tr><td rowspan=1 colspan=2>G-2 Detailed DesignStandrds</td><td></td><td></td><td rowspan=1 colspan=1></td><td rowspan=2 colspan=1>Phase 5: Post-Implementation</td><td rowspan=2 colspan=1></td></tr><tr><td rowspan=2 colspan=2></td><td rowspan=1 colspan=3>G-3 Noise Standards</td><td></td><td></td></tr><tr><td rowspan=1 colspan=3>Mean/Method of Complince</td><td rowspan=5 colspan=2></td><td rowspan=5 colspan=1>Wake SeparationDetermination</td><td rowspan=3 colspan=1>Develop performance data packagee.gei,fightcmandcontrolperformanceetc.)</td></tr><tr><td rowspan=1 colspan=2>CompliancePlanning</td><td rowspan=1 colspan=3>Review and Acceptance ofCertication Plans</td></tr><tr><td rowspan=7 colspan=2>Implementation</td><td rowspan=2 colspan=3>Conformity Inspections</td></tr><tr><td rowspan=1 colspan=1>Wake Separation Assessment</td></tr><tr><td rowspan=1 colspan=3>Detail-level compliance plan</td><td rowspan=1 colspan=2></td><td rowspan=1 colspan=1>Update 7360.1</td></tr><tr><td rowspan=2 colspan=3>Product-level complance plan</td><td rowspan=6 colspan=2></td><td rowspan=6 colspan=1>Community/StakeholderEngagement</td><td rowspan=1 colspan=1>Messaging development</td></tr><tr><td rowspan=1 colspan=1>Website development</td></tr><tr><td rowspan=1 colspan=3>Safety Review Board</td><td rowspan=2 colspan=1>Continued Regional Office CommunityEnagflnroundtables)</td></tr><tr><td rowspan=1 colspan=3>TIA &amp; Conformity Inspecion</td></tr><tr><td rowspan=3 colspan=2></td><td rowspan=2 colspan=3>Filight Testss</td><td rowspan=2 colspan=2></td><td></td></tr><tr><td rowspan=1 colspan=1>Airspace Implementation CommunityEngagement</td></tr><tr><td rowspan=1 colspan=3>Type Inpection Report</td><td rowspan=1 colspan=2></td><td></td><td></td></tr><tr><td></td><td></td><td rowspan=4 colspan=3>Final Type Certification Board</td><td></td><td></td><td></td><td></td></tr><tr><td></td><td></td><td></td><td rowspan=3 colspan=1></td><td rowspan=3 colspan=1>Airline Crew Preparation</td><td></td></tr><tr><td rowspan=3 colspan=2></td><td></td><td></td></tr><tr><td></td><td rowspan=1 colspan=1>Identify, vet, nd train e</td></tr><tr><td rowspan=1 colspan=3>Isse Type Cericate</td><td></td><td rowspan=2 colspan=1></td><td rowspan=2 colspan=1>Site-specific AAMforecast</td><td rowspan=2 colspan=1></td></tr><tr><td rowspan=2 colspan=2>Post CertificationActivities</td><td rowspan=2 colspan=3></td><td rowspan=2 colspan=2></td></tr><tr><td rowspan=1 colspan=1>Rulemaking</td><td rowspan=1 colspan=1>Rulemaking for Pilo TrainingPowered-lift NPRM</td></tr></table>

## 7 AAM Evolution Framework

The FAA’s approach to supporting the operationalization of AAM encompasses a series of incremental changes and advancements to the regulatory, technological, and operational frameworks that govern the NAS. This approach aims to ensure safety, while also facilitating efficiency and innovation in the AAM industry and will result in a continuum of AAM capabilities that evolves over time as the tempo of operations increases, driving the need for more advanced supporting infrastructure, regulations, and processes. This will allow the collection of early benefits and lessons learned while maintaining progress toward the fully mature state of AAM.

The agency is working on a regulatory framework that will allow AAM aircraft to be fully integrated into the airspace and operate alongside traditional aircraft in the near-term and beyond. The FAA and industry are developing the necessary technologies to support AAM operations, including aircraft and traffic management systems, communication networks, and autonomous capabilities. Finally, the FAA is working to establish operational frameworks that ensure the safe integration of AAM aircraft into the NAS, including training pilots, air traffic controllers, and other stakeholders on new procedures and regulations.

This evolutionary approach to AAM provides advantages. By initially supporting lower complexity operations in the near-term, as with I28, implementation can be achieved by maximizing the use of current capabilities that meet performance requirements and do not require full-scale regulatory and operational infrastructure changes.

With increased tempo, AAM operations will evolve through changes to governing regulations augmented by AAM infrastructure, automation, and cooperative traffic management practices supported by third party services. The evolution to a collaborative, information-rich, data-sharing environment will require new technologies and capabilities. AAM operators and other stakeholders will share information with the FAA having ondemand access to information as needed.

The FAA’s ANG organization developed an initial AAM framework that categorizes the evolving phases of AAM and provides context on the AAM roadmap to operationalization. The framework describes the anticipated operational capabilities for both FAA and industry stakeholders as the AAM ecosystem develops and matures over time. The framework also serves to identify key areas that require prioritization and coordination among the various stakeholders across the AAM ecosystem. The framework will inform FAA efforts, but also can be used by industry and other government agencies.

## AAM Coordination Areas

The AAM framework consists of five high-level coordination areas, shown in Table 2, within which key AAM capabilities pertaining to both FAA and industry stakeholders are highlighted. AAM capabilities are expected to progress independently toward a mature state. The pace of development may vary within and between coordination areas. Maturity is capability dependent, and not bound by a specific timeline. Regional maturity rates may vary as well, with some communities embracing AAM operations more rapidly than others.

It should be noted that community engagement, although not shown here, will be an integral and required step for each coordination area.

Table 2. AAM Coordination Areas
<table><tr><td rowspan=1 colspan=1>Area</td><td rowspan=1 colspan=1>Considerations for FAA and Industry Stakeholders</td></tr><tr><td rowspan=1 colspan=1>Aircraft System</td><td rowspan=1 colspan=1>Aircraft, equipment, automation, certification</td></tr><tr><td rowspan=1 colspan=1>Infrastructure</td><td rowspan=1 colspan=1>Facilities, data systems related standards, federated networks, CNS</td></tr><tr><td rowspan=1 colspan=1>Operations</td><td rowspan=1 colspan=1>Operational density and modes, procedures, pilot knowledge and training</td></tr><tr><td rowspan=1 colspan=1>Airspace</td><td rowspan=1 colspan=1>Routes, waivers, cooperative areas, charting and publication</td></tr><tr><td rowspan=1 colspan=1>ATC Procedures</td><td rowspan=1 colspan=1>Standard operating procedures, LOAs, public-private responsibilities</td></tr></table>

## AAM Maturity Levels

The evolution of capabilities addresses initial, intermediate, and mature states of AAM, and is described across six maturity levels (0-5). Each maturity level is characterized by a set of expected outcomes, as shown in Table 3. One or more triggering events indicate progression from one maturity level to the next.

Table 3. AAM Maturity Levels
<table><tr><td rowspan=1 colspan=1>Level</td><td rowspan=1 colspan=1>Description</td><td rowspan=1 colspan=1>Trigger Events (for reaching level)</td></tr><tr><td rowspan=1 colspan=1>0</td><td rowspan=1 colspan=1>Late-stage certification testing in limitedenvironments, aircraft certification testing andoperational evaluations with conformingprototypes and existing rules/procedures, andearly industry development and prototyping.</td><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>1</td><td rowspan=1 colspan=1>Exploratory operations of minimal density andcomplexity, type certified aircraft, early FAAprocedures development, and initial Provider of Services for UAM (PSU) services.</td><td rowspan=1 colspan=1>Completion of relevant NPRMs andrulemaking to allow for vehicle typecertification, initial public standards to supportdata exchanges between industry participantsand the FAA.</td></tr><tr><td rowspan=1 colspan=1>2</td><td rowspan=1 colspan=1>Low-density scheduled commercial operations in urban areas and aroundairports, as well as an established federatedservice network* with several PSUs andSupplementary Data Service Providers(SDSPs). Designated cooperative airspace islimited (see UAM ConOps, Version 2.0).*A federated service network is one that isprovided and supported by the operators andthird-party service providers to exchange the information and agreements needed for FAA-approved cooperative operating practices.</td><td rowspan=1 colspan=1>Increased operational density, newoperational modes (e.g., remotely piloted),and the evaluation of cooperative airspaceand a federated service network with multipleoperating PSUs.</td></tr><tr><td rowspan=1 colspan=1>3</td><td rowspan=1 colspan=1>Medium-density scheduled and unscheduledcommercial operations using an increasednumber of vertiports and routes in specificgeographical areas that make continued use of limited, designated cooperative airspace.Established PSUs and federated servicenetworks support increased levels ofautomation and instances of remotely pilotedaircraft with a safety pilot on board.</td><td rowspan=1 colspan=1>Continued evolution of the modes ofoperations, implementation of designatedcooperative airspace in more geographicalareas, and the establishment of certificationstandards for automated and remotelyoperated large aircraft.</td></tr><tr><td rowspan=1 colspan=1>4</td><td rowspan=1 colspan=1> Medium-density scheduled and unscheduledcommercial operations in an AAM networkthat make widespread use of cooperativeairspace. Fully remotely-piloted operationsare supported.</td><td rowspan=1 colspan=1>Certification of fully remote piloted aircraftand the availability of enhanced CNScapabilities that can support long distanceand fully remote operations, complete implementation of new regulatory frameworks, widespread implementation ofcooperative airspace and vertiports, and theability to support operations in instrumentmeteorological conditions (IMC).</td></tr><tr><td rowspan=1 colspan=1>5</td><td rowspan=1 colspan=1> Mature AAM ecosystem, characterized byhigh density scheduled, unscheduled, andon-demand operations that aregeographically dispersed and served byaircraft able to operate autonomously.</td><td rowspan=1 colspan=1>Certification of fully autonomous aircraft andthe satisfactory performance of highlyintegrated automation within the federatedservice network.</td></tr></table>

## FAA and Industry Coordination

The AAM evolution framework embraces independent advancement within coordination areas, but also acknowledges the need for coordination across the areas for the AAM ecosystem to come to fruition. It considers both FAA and industry activities and capabilities to support AAM maturation.

## Rulemaking

The FAA uses the same rulemaking process for AAM operations as it does for other aviation-related regulations. To carry out its responsibilities, the FAA must issue regulations that are clear and provide direction to the aviation industry and the public. Through the rulemaking process, the FAA engages with stakeholders, including industry groups, pilots, and the public, to develop regulations that are informed by their inputs. The process provides an opportunity for all interested parties to provide comments and feedback on proposed regulations, which helps to ensure that the final regulations are effective, practical, and above all, ensure safety.

## Standards Development

Industry stakeholders, including aircraft manufacturers, operators, and infrastructure providers, play a critical role in developing standards for AAM operations. Industry-driven standards are essential to ensure that AAM vehicles and infrastructure are safe, reliable, and interoperable. Long lead times and the level of stakeholder participation required to develop standards is a high priority area that requires establishing relationships among all the stakeholders, identifying standards development needs, and generating multi-year plans to address those needs and associated actions.

## Technology Development and Deployment

Industry’s development of technology often moves faster than the regulations addressing the use of the technologies. The FAA needs to establish and maintain close ties with industry to ensure that emerging technologies are designed with safety and NAS integration in mind and that regulations do not unduly constrain technology and market development. This includes the need for industry to consider the complexity of aviation operations and human factors, especially when proposing highly automated solutions. Additionally, the FAA needs to work closely with foreign regulatory counterparts and Air Navigation Service Providers to align and harmonize AAM-related regulations, policies and procedures, as applicable, given this sector’s global, entrepreneurial, and innovative ecosystem.

The long lead time for development and deployment of FAA capabilities also makes identifying FAA technology/capability requirements and establishing roadmaps for acquisition and development a high priority activity.

## Network Development

The mature state vision for AAM involves industry-built networks for data exchange to support many functions that the FAA has traditionally performed, including aspects of airspace management. These networks and the processes implemented for using them must be compatible with FAA data exchange mechanisms and airspace design and procedures.

## Airspace Design and Management

Initial AAM operations that are low density and low complexity will be conducted using existing airspace design and charting processes, and airspace constructs available today (e.g., VFR corridors/flyways, T-routes). As the operations continue to increase in volume and complexity, novel airspace design may be needed to accommodate operations. The concept of designating cooperative areas for AAM operations envisions safe and efficient operations that may not require traditional ATC services in certain situations. They will be available to any aircraft appropriately equipped to meet the performance requirements and are created and implemented when operationally advantageous.

## Moving Forward

The FAA will continue to work with AAM stakeholders to refine and further mature this framework and move towards an AAM ecosystem that supports innovation and scalability. The FAA is committed to ensuring the appropriate resources are allocated, workgroups are established to address areas that require research and development, and policy and regulatory decisions keep AAM moving forward into the future.

## Acronyms

<table><tr><td rowspan=1 colspan=1>Acronym</td><td rowspan=1 colspan=1>Definition</td><td rowspan=1 colspan=1>Acronym</td><td rowspan=1 colspan=1>Definition</td></tr><tr><td rowspan=1 colspan=1>AAM</td><td rowspan=1 colspan=1>Advanced Air Mobility</td><td rowspan=1 colspan=1>IMC</td><td rowspan=1 colspan=1>Instrument Meteorological Conditions</td></tr><tr><td rowspan=1 colspan=1>AC</td><td rowspan=1 colspan=1>Advisory Circular</td><td rowspan=1 colspan=1>IMS</td><td rowspan=1 colspan=1> Integrated Master Schedule</td></tr><tr><td rowspan=1 colspan=1>ADS-B</td><td rowspan=1 colspan=1>Automatic Dependent Surveillance-Broadcast</td><td rowspan=1 colspan=1>128</td><td rowspan=1 colspan=1>Innovate28</td></tr><tr><td rowspan=1 colspan=1>AGC</td><td rowspan=1 colspan=1>Office of the Chief Counsel</td><td rowspan=1 colspan=1>LOA</td><td rowspan=1 colspan=1>Letter of Agreement</td></tr><tr><td rowspan=1 colspan=1>AEE</td><td rowspan=1 colspan=1>Office of Environment and Energy</td><td rowspan=1 colspan=1>LOB</td><td rowspan=1 colspan=1>Line of Business</td></tr><tr><td rowspan=1 colspan=1>AFX</td><td rowspan=1 colspan=1>Flight Standards Service</td><td rowspan=1 colspan=1>MOC</td><td rowspan=1 colspan=1>Means of Compliance</td></tr><tr><td rowspan=1 colspan=1>AIM</td><td rowspan=1 colspan=1>Aeronautical Information Manual</td><td rowspan=1 colspan=1>MOU</td><td rowspan=1 colspan=1>Memorandum of Understanding</td></tr><tr><td rowspan=1 colspan=1>AIP</td><td rowspan=1 colspan=1>Aeronautical Information Publication</td><td rowspan=1 colspan=1>NAS</td><td rowspan=1 colspan=1>National Airspace System</td></tr><tr><td rowspan=1 colspan=1>AIR</td><td rowspan=1 colspan=1>Aircraft Certification Service</td><td rowspan=1 colspan=1>NASA</td><td rowspan=1 colspan=1>National Aeronautics and SpaceAdministration</td></tr><tr><td rowspan=1 colspan=1>ANG</td><td rowspan=1 colspan=1>Office of NextGen</td><td rowspan=1 colspan=1>NEPA</td><td rowspan=1 colspan=1>National Environmental Policy Act</td></tr><tr><td rowspan=1 colspan=1>ARC</td><td rowspan=1 colspan=1>Aviation Rulemaking Committee</td><td rowspan=1 colspan=1>NOTAM</td><td rowspan=1 colspan=1>Notice to Air Mission</td></tr><tr><td rowspan=1 colspan=1>ARP</td><td rowspan=1 colspan=1>Ooffice of Airports</td><td rowspan=1 colspan=1>NREL</td><td rowspan=1 colspan=1>National Renewable Energy Lab</td></tr><tr><td rowspan=1 colspan=1>ASOS</td><td rowspan=2 colspan=1>Automated Surface ObservingSystem</td><td rowspan=2 colspan=1>NTSB</td><td rowspan=2 colspan=1>National Transportation Safety Board</td></tr><tr><td rowspan=1 colspan=1></td></tr><tr><td rowspan=1 colspan=1>ATC</td><td rowspan=1 colspan=1>Air Traffic Control</td><td rowspan=1 colspan=1>OEM</td><td rowspan=1 colspan=1>Original Equipment Manufacturer</td></tr><tr><td rowspan=1 colspan=1>ATM</td><td rowspan=1 colspan=1>Air Traffic Management</td><td rowspan=1 colspan=1>NPRM</td><td rowspan=1 colspan=1>Notice of Proposed Rulemaking</td></tr><tr><td rowspan=1 colspan=1>ATO</td><td rowspan=1 colspan=1>Air Traffic Organization</td><td rowspan=1 colspan=1>PHMSA</td><td rowspan=1 colspan=1>Pipeline and Hazardous Materials SafetyAdministration</td></tr><tr><td rowspan=1 colspan=1>ATR</td><td rowspan=1 colspan=1>Airport Technology Research andDevelopment Branch</td><td rowspan=1 colspan=1>PIC</td><td rowspan=1 colspan=1>Pilot in Command</td></tr><tr><td rowspan=1 colspan=1>AWOS</td><td rowspan=1 colspan=1>Automated Weather ObservingSystem</td><td rowspan=1 colspan=1>PSU</td><td rowspan=1 colspan=1>Provider of Services for Urban Air Mobility</td></tr><tr><td rowspan=1 colspan=1>CFR</td><td rowspan=1 colspan=1>Code of Federal Regulations</td><td rowspan=1 colspan=1>SDSP</td><td rowspan=1 colspan=1>Supplementary Data Service Provider</td></tr><tr><td rowspan=1 colspan=1>CNS</td><td rowspan=1 colspan=1>Communications NavigationSurveillance</td><td rowspan=1 colspan=1>SFAR</td><td rowspan=1 colspan=1>Special Federal Aviation Regulation</td></tr><tr><td rowspan=1 colspan=1>DOT</td><td rowspan=1 colspan=1>Department of Transportation</td><td rowspan=1 colspan=1>SFRA</td><td rowspan=1 colspan=1>Special Flight Rules Area</td></tr><tr><td rowspan=1 colspan=1>EB</td><td rowspan=1 colspan=1>Engineering Brief</td><td rowspan=1 colspan=1>SMS</td><td rowspan=1 colspan=1>Safety Management System</td></tr><tr><td rowspan=1 colspan=1>EIS</td><td rowspan=1 colspan=1>Entry into Service</td><td rowspan=1 colspan=1>STOL</td><td rowspan=1 colspan=1>Short Takeff and Landing</td></tr><tr><td rowspan=1 colspan=1>EMS</td><td rowspan=1 colspan=1>Emergency Management Services</td><td rowspan=1 colspan=1>TFR</td><td rowspan=1 colspan=1>Temporary Flight Restriction</td></tr><tr><td rowspan=1 colspan=1>eVTOL</td><td rowspan=1 colspan=1>Electric Vertical Takeoff and Landing</td><td rowspan=1 colspan=1>TLOF</td><td rowspan=1 colspan=1>Touchdown and Liftoff Area</td></tr><tr><td rowspan=1 colspan=1>FAA</td><td rowspan=1 colspan=1>Federal Aviation Administration</td><td rowspan=1 colspan=1>UAM</td><td rowspan=1 colspan=1>Urban Air Mobility</td></tr><tr><td rowspan=1 colspan=1>GA</td><td rowspan=1 colspan=1>General Aviation</td><td rowspan=1 colspan=1>U.S.C.</td><td rowspan=1 colspan=1>United States Code</td></tr><tr><td rowspan=1 colspan=1>HMR</td><td rowspan=1 colspan=1>Hazardous Materials Regulation</td><td rowspan=1 colspan=1>VMC</td><td rowspan=1 colspan=1>Visual Meteorological Conditions</td></tr><tr><td rowspan=1 colspan=1>ICAO</td><td rowspan=1 colspan=1>International Civil AviationOrganization</td><td rowspan=1 colspan=1>VFR</td><td rowspan=1 colspan=1>Visual Flight Rules</td></tr></table>