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ASTM F3423/F3423M-22

(Specification)

Standard Specification for Vertiport Design

Standard Specification for Vertiport Design

SCOPE
1.1 This specification defines the requirements for the planning, design, and establishment of vertiports intended to service vertical takeoff and landing (VTOL) aircraft. These aircraft include, but are not limited to, standard category aircraft, optionally piloted aircraft, and unmanned aircraft. Aircraft not covered by this specification include VTOL aircraft less than 55 lb [25 kg]. In developing these standards, identified types of eVTOL aircraft, for example, Multi-Rotor, Lift & Cruise, Vectored Thrust, Tilt Wing, Tilt Rotor, etc., were considered. Ultimately it is up to the authorities having jurisdiction (AHJ) as to how and to what extent these standards are applied. Vertiports may provide commercial or private services in support of the operation of eVTOL aircraft including, but not limited to, some or all of occupant and cargo transport, air medical, flight instruction, aerial work, aircraft rental, fueling, charging of energy storage devices, battery exchange, hangaring, and maintenance services.  
1.2 This specification is intended to support the design of civil vertiports and vertistops, however, it may also be used as a best practice document for other facilities.  
1.2.1 Vertiport  is a generic reference to the area of land, water, or structure used, or intended to be used, for the landing and takeoff of VTOL aircraft, together with associated buildings and facilities. At this time, aircraft with floats conducting water landings and takeoffs are not included in this specification.  
1.2.2 Vertistop—The same as Vertiport, except that no fueling, defueling, scheduled maintenance, scheduled repairs, or storage of aircraft is permitted. Unscheduled maintenance and repairs to return an aircraft in an AOG (Aircraft on Ground) status to a serviceable status are permissible.  
1.3 This document may present information in either SI units, English Engineering units, or both. The values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined  
1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.  
1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

General Information

Status
Published
Publication Date
30-Jun-2022
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F38 - Unmanned Aircraft Systems
Drafting Committee
F38.02 - Flight Operations
Current Stage
Ref Project

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ASTM F3423/F3423M-22 - Standard Specification for Vertiport DesignASTM F3423/F3423M-22 - Standard Specification for Vertiport Design
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ASTM F3423/F3423M-22 - Standard Specification for Vertiport Design
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Standards Content (Sample)

This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Designation: F3423/F3423M −22
Standard Specification for
1
Vertiport Design
ThisstandardisissuedunderthefixeddesignationF3423/F3423M;thenumberimmediatelyfollowingthedesignationindicatestheyear
of original adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.
A superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope 1.4 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
1.1 This specification defines the requirements for the
responsibility of the user of this standard to establish appro-
planning, design, and establishment of vertiports intended to
priate safety, health, and environmental practices and deter-
service vertical takeoff and landing (VTOL) aircraft. These
mine the applicability of regulatory limitations prior to use.
aircraft include, but are not limited to, standard category
1.5 This international standard was developed in accor-
aircraft, optionally piloted aircraft, and unmanned aircraft.
dance with internationally recognized principles on standard-
Aircraft not covered by this specification include VTOL
ization established in the Decision on Principles for the
aircraft less than 55lb [25kg]. In developing these standards,
Development of International Standards, Guides and Recom-
identified types of eVTOL aircraft, for example, Multi-Rotor,
mendations issued by the World Trade Organization Technical
Lift&Cruise,VectoredThrust,TiltWing,TiltRotor,etc.,were
Barriers to Trade (TBT) Committee.
considered. Ultimately it is up to the authorities having
jurisdiction(AHJ)astohowandtowhatextentthesestandards
2. Referenced Documents
are applied. Vertiports may provide commercial or private
2
2.1 ASTM Standards:
services in support of the operation of eVTOL aircraft
F3060Terminology for Aircraft
including,butnotlimitedto,someorallofoccupantandcargo
F3341/F3341MTerminology for Unmanned Aircraft Sys-
transport, air medical, flight instruction, aerial work, aircraft
tems
rental, fueling, charging of energy storage devices, battery
3
exchange, hangaring, and maintenance services.
2.2 AIA Standards:
NASNational Aerospace Standards
1.2 This specification is intended to support the design of
4
civil vertiports and vertistops, however, it may also be used as
2.3 FAA Standards:
a best practice document for other facilities. 14 CFR Part 77Safe, Efficient Use and Preservation of the
1.2.1 Vertiport is a generic reference to the area of land,
Navigable Airspace
water, or structure used, or intended to be used, for the landing
14 CFR Part 157 Notice of Construction, Alteration,
and takeoff of VTOL aircraft, together with associated build-
Activation, and Deactivation of Airports
ings and facilities.At this time, aircraft with floats conducting
AIMAeronautical Information Manual
water landings and takeoffs are not included in this specifica-
FAAPilot/Controller Glossary
tion.
FSIMS 8900.1Vol 8, Ch 3, Sec 3 Evaluation and Surveil-
1.2.2 Vertistop—The same as Vertiport, except that no
lance of Heliports
fueling, defueling, scheduled maintenance, scheduled repairs,
AC 00-34AAircraft Ground Handling and Servicing
or storage of aircraft is permitted. Unscheduled maintenance
AC 70/7460Obstruction Marking and Lighting
and repairs to return an aircraft in an AOG (Aircraft on
AC 150/5200-33BHazardous Wildlife Attractants on or
Ground) status to a serviceable status are permissible.
Near Airports
AC 150/5345-27ESpecification for Wind Cone Assemblies
1.3 This document may present information in either SI
AC 150/5390Heliport Design Guide
units, English Engineering units, or both. The values stated in
Order JO 6700.20BNon-Federal Navigational Aids, Air
each system are not necessarily exact equivalents; therefore, to
ensure conformance with the standard, each system shall be
used independently of the other, and values from the two
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
systems shall not be combined
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on
1
This specification is under the jurisdiction of ASTM Committee F38 on the ASTM website.
3
UnmannedAircraftSystemsandisthedirectresponsibilityofSubcommitteeF38.02 Available from Aerospace Industries Association (AIA), 1000 Wilson Blvd.,
on Flight Operations. Suite 1700, Arlington, VA 22209, http://www.aia-aerospace.org.
4
Current edition approved July 1, 2022. Published August 2022. DOI: 10.1520/ Available from Federal Aviation Administration (FAA), 800 Independence
F3423_
...

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1.1 This standard practice establishes the minimum set of requirements for auditing programs, methods, and systems, the responsibilities for all parties involved, and qualifications for entities conducting audits against ASTM standards on Unmanned Aircraft Systems. This document has been purposefully designed within the broader context of the Committee F38 library. Although the original source materials for the content presented here were intended to function as standalone documents, the committee has consciously removed any redundant information in favor of adopting a referential "single-source-of-truth" approach. Consequently, when applying this standard, it is essential to consider and integrate all relevant Committee F38 standards to ensure its comprehensive and accurate implementation.  
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1.1 This specification provides the minimum requirements for an Unmanned Aircraft Flight Manual (UFM) for an unmanned aircraft system (UAS) designed, manufactured, and operated in the light UAS category as defined by a Civil Aviation Authority (CAA). Depending on the size and complexity of the UAS, an UFM may also contain the instruction for maintenance and continuing airworthiness for owner / operator authorized maintenance. This document has been purposefully designed within the broader context of the Committee F38 library. Although the original source materials for the content presented here were intended to function as standalone documents, the committee has consciously removed any redundant information in favor of adopting a referential "single-source-of-truth" approach. Consequently, when applying this standard, it is essential to consider and integrate all relevant Committee F38 standards to ensure its comprehensive and accurate implementation.  
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Standard Practice for Independent Audit Program for Unmanned Aircraft Operators

SIGNIFICANCE AND USE
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Standard Guide for Training for Remote Pilot in Command of Unmanned Aircraft Systems (UAS) Endorsement

SIGNIFICANCE AND USE
4.1 The purpose of this guide is to provide a standardized means of facilitating Remote Pilot training. The guide should be used by all individuals and agencies that train such persons.  
4.2 Successful completion of this training course neither constitutes nor implies certification or licensure from the CAA.  
4.3 This guide is intended to provide guidance to:  
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This specification establishes the design, construction, and test requirements for a small unmanned aircraft system (sUAS). It is intended for all sUAS that are permitted to operate over a defined area and in airspace authorized by a nation's governing aviation authority (GAA). Unless otherwise specified by a nation’s GAA, this specification applies only to UA that have a maximum takeoff gross weight of 55 lb/25 kg or less.
SCOPE
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1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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ASTM F3411-22a(Specification)
Standard Specification for Remote ID and Tracking

SCOPE
1.1 This specification covers the performance requirements for remote identification (Remote ID) of unmanned aircraft systems (UAS). Remote ID allows governmental and civil identification of UAS for safety, security, and compliance purposes. The objective is to increase UAS remote pilot accountability by removing anonymity while preserving operational privacy for remote pilots, businesses, and their customers. Remote ID is an enabler of enhanced operations such as beyond visual line of sight (BVLOS) operations as well as operations over people.  
1.2 This specification defines message formats, transmission methods, and minimum performance standards for two forms of Remote ID: broadcast and network. Broadcast Remote ID is based on the transmission of radio signals directly from a UAS to receivers in the UAS’s vicinity. Network Remote ID is based on communication by means of the internet from a network Remote ID service provider (Net-RID SP) that interfaces directly or indirectly with the UAS, or with other sources in the case of intent-based network participants.  
1.3 This specification addresses the communications and test requirements of broadcast or network Remote ID, or both, in UAS and Net-RID SP systems.  
1.4 Applicability:  
1.4.1 This specification is applicable to UAS that operate at very low level (VLL) airspace over diverse environments including but not limited to rural, urban, networked, network degraded, and network denied environments, regardless of airspace class.  
1.4.2 This specification neither purports to address UAS operating with approval to use ADS-B or secondary surveillance radar transponders, nor does it purport to solve ID needs of UAS for all operations.  
1.4.3 In particular, this specification does not purport to address identification needs for UAS that are not participating in Remote ID or operators that purposefully circumvent Remote ID.  
1.5 The values stated in SI units are to be regarded as standard. The values given in parentheses after SI units are provided for information only and are not considered standard.  
1.5.1 Units of measurement included in this specification:    
m  
meters  
deg, °  
degrees of latitude and longitude, compass direction  
s  
seconds  
Hz  
Hertz (frequency)  
dBm  
decibel-milliwatts (radio frequency power)  
ppm  
parts per million (radio frequency variation)  
μs  
microseconds  
ms  
milliseconds  
1.6 Table of Contents:    
Title  
Section  
Scope  
1  
Referenced Documents  
2  
Terminology  
3  
Remote ID and Network Interoperability Conceptual Overview  
4  
Performance Requirements  
5  
TEST METHODS  
Scope  
6  
Significance and Use  
7  
Hazards  
8  
Test Units  
9  
Procedure  
10  
Precision and Bias  
11  
Product Marking  
12  
Packaging and Package Marking  
13  
Keywords  
14  
ANNEX A1—Broadcast Authentication Verifier Service  
Annex A1  
ANNEX A2—Network Remote ID Interoperability Requirements, APIs, and Testing  
Annex A2  
ANNEX A3—Tables of Values  
Annex A3  
ANNEX A4—USS-DSS and USS-USS OpenAPI YAML Description  
Annex A4  
ANNEX A5—Number Registrar Management Policy  
Annex A5  
APPENDIX X1—Performance Characteristics  
Appendix X1  
APPENDIX X2—List of Subcommittee Participants and Contributors  
Appendix X2  
APPENDIX X3—Background Information  
Appendix X3  
1.7 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. Some specific hazards statements are given in Section 8 on Hazards.  
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ASTM F3586-22(Practice)
Standard Practice for Remote ID Means of Compliance to Federal Aviation Administration Regulation 14 CFR Part 89

SIGNIFICANCE AND USE
3.1 The general approach to this practice is to serve as an “overlay” of requirements to the ASTM F3411-22a Standard Specification for Remote ID and Tracking by identifying mandatory portions, substituting values as needed, overriding items that may be optional, and providing additional requirements that are beyond the scope of Specification F3411, yet are necessary to provide proper guidance to meet the requirements set forth in Part 89.  
3.2 Furthermore, this practice provides additional details on minimal testing requirements for those submitting a DOC based on this MOC.
SCOPE
1.1 This practice provides a Means of Compliance (MOC) that gives sufficient clarity to the Unmanned Aircraft System (UAS) or Broadcast Module manufacturers to produce a compliant Remote ID (RID) System (RIDS) such that submitting a Declaration of Compliance2 (DOC) to this MOC will satisfy the requirements of the Federal Aviation Administration (FAA) 14 CFR Part 89 (Part 89) rule.3 This practice also explains what to expect from aircraft operating in compliance to this MOC.  
1.2 The FAA provided three options to comply with the Remote ID regulations: Standard Remote ID UAS, Remote ID Broadcast Modules, and FAA-recognized identification areas (FRIAs). The scope of this MOC is to cover both Standard RID and RID Broadcast Modules.  
1.3 The FRIA portion of the rule is out of scope since it provides a means to avoid the technical RID requirements by operating within administrative boundaries.  
1.4 Both SI and non-SI units are used in this document. Since this is an aviation standard and it addresses FAA rules, some units are used in preference of being consistent with industry and regulatory norms.  
1.5 Table of Contents:    
Title  
Section  
Scope  
1  
Referenced Documents  
2  
Significance and Use  
3  
Subset of Options in the F3411 Specification Considered  
4  
Requirements and Exceptions from the F3411 Specification  
5  
Alternative Applications of Specification F3411 to Meet Part 89
Requirements  
6  
MOC Requirements Not Covered by the Practice  
7  
Test Methods  
8  
Precision and Bias  
9  
Satisfaction of Rule Requirements  
10  
Keywords  
11  
ANNEX A1—Simulation Option for Accuracy Testing  
Annex A1  
APPENDIX X1—External Device for GCS Location Source Rationale  
Appendix X1  
APPENDIX X2—Power Level Rationale  
Appendix X2  
1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.  
1.7 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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