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ASTM F3366-19

(Specification)

Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)

Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)

SCOPE
1.1 This specification provides the minimum requirements for a General Maintenance Manual (GMM) for an unmanned aircraft system (UAS) designed, manufactured, and operated in the small UAS category as defined by a Civil Aviation Authority (CAA).  
1.2 This specification applies to support professional entities that will receive operator certification by a CAA, and provide standards of practice for self- or third-party audit of operators of UAS.  
1.3 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.  
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-Apr-2019
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F38 - Unmanned Aircraft Systems
Drafting Committee
F38.03 - Personnel Training, Qualification and Certification
Current Stage
Ref Project

Relations

Refers
ASTM F3298-18 - Standard Specification for Design, Construction, and Verification of Fixed-Wing Unmanned Aircraft Systems (UAS)
Effective Date
01-May-2018
Refers
ASTM F2908-16 - Standard Specification for Aircraft Flight Manual (AFM) for a Small Unmanned Aircraft System (sUAS)
Effective Date
15-Feb-2016
Refers
ASTM F3298-19 - Standard Specification for Design, Construction, and Verification of Lightweight Unmanned Aircraft Systems (UAS)
Effective Date
01-Feb-2019
Refers
ASTM F2909-19 - Standard Specification for Continued Airworthiness of Lightweight Unmanned Aircraft Systems
Effective Date
01-Sep-2019
Referred By
ASTM F3341/F3341M-23 - Standard Terminology for Unmanned Aircraft Systems
Effective Date
01-May-2019
Referred By
ASTM F3600-22 - Standard Guide for Unmanned Aircraft System (UAS) Maintenance Technician Qualification
Effective Date
01-May-2019

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ASTM F3366-19 - Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)ASTM F3366-19 - Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)
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ASTM F3366-19 - Standard Specification for General Maintenance Manual (GMM) for a small Unmanned Aircraft System (sUAS)
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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: F3366 −19
Standard Specification for
General Maintenance Manual (GMM) for a small Unmanned
1
Aircraft System (sUAS)
This standard is issued under the fixed designation F3366; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope F2910 Specification for Design and Construction of a Small
Unmanned Aircraft System (sUAS)
1.1 This specification provides the minimum requirements
F2911 Practice for Production Acceptance of Small Un-
for a General Maintenance Manual (GMM) for an unmanned
manned Aircraft System (sUAS)
aircraft system (UAS) designed, manufactured, and operated in
F3002 Specification for Design of the Command and Con-
the small UAS category as defined by a Civil Aviation
trolSystemforSmallUnmannedAircraftSystems(sUAS)
Authority (CAA).
F3003 Specification for Quality Assurance of a Small Un-
1.2 This specification applies to support professional enti-
manned Aircraft System (sUAS)
ties that will receive operator certification by a CAA, and
F3005 Specification for Batteries for Use in Small Un-
provide standards of practice for self- or third-party audit of
manned Aircraft Systems (sUAS)
operators of UAS.
F3298 Specification for Design, Construction, and Verifica-
tion of Lightweight Unmanned Aircraft Systems (UAS)
1.3 The values stated in inch-pound units are to be regarded
3
as standard. The values given in parentheses are mathematical 2.2 Federal Standards:
conversions to SI units that are provided for information only 14 CFR Part 43 Maintenance, Preventive Maintenance,
and are not considered standard. Rebuilding, and Alteration
14 CFR Part 107 Small Unmanned Aircraft Systems
1.4 This standard does not purport to address all of the
4
2.3 Military Standard:
safety concerns, if any, associated with its use. It is the
MIL-STD-3001 Preparation of Digital Technical Informa-
responsibility of the user of this standard to establish appro-
tion for Multi-Output Presentation of Technical Manuals
priate safety, health, and environmental practices and deter-
mine the applicability of regulatory limitations prior to use.
3. Terminology
1.5 This international standard was developed in accor-
dance with internationally recognized principles on standard- 3.1 Definitions:
3.1.1 applicant/proponent, n—the person or organization
ization established in the Decision on Principles for the
Development of International Standards, Guides and Recom- responsible for seeking the approval to operate and operating a
UA. The applicant/proponent may be one of the following
mendations issued by the World Trade Organization Technical
Barriers to Trade (TBT) Committee. entities: manufacturer, operator, or original equipment manu-
facturer.
2. Referenced Documents
3.1.1.1 manufacturer, n—the person or organization who
2
causes production of a product or article. A manufacturer may
2.1 ASTM Standards:
also be an operator.
F2908 Specification for Unmanned Aircraft Flight Manual
(UFM) for an Unmanned Aircraft System (UAS)
3.1.1.2 operator, n—the person or organization who applies
F2909 Practice for Maintenance and Continued Airworthi-
for CAA approval to operate a UAS or who seeks operational
ness of Small Unmanned Aircraft Systems (sUAS)
approval for types of flight operations prohibited by a CAAfor
that UAS.
3.1.1.3 original equipment manufacturer (OEM), n—the
1
This specification is under the jurisdiction of ASTM Committee F38 on
person or organization who first produced that product or
UnmannedAircraftSystemsandisthedirectresponsibilityofSubcommitteeF38.03
article. An OEM may also be an operator.
on Personnel Training, Qualification and Certification.
Current edition approved May 1, 2019. Published June 2019. DOI: 10.1520/
F3366–19.
2 3
For referenced ASTM standards, visit the ASTM website, www.astm.org, or Available from U.S. Government Publishing Office, 732 N. Capitol St., NW,
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Washington, DC 20401, http://www.gpo.gov.
4
Standards volume information, refer to the standard’s Document Summary page on Available from DLA Document Services, Building 4/D, 700 Robbins Ave.,
the ASTM website. Philadelphia, PA 19111-5094, http://quicksearch.dla.mil.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3366 − 19
3.1.2 field maintenance, n—inspections and repairs made by 3.2.8 UA—Unmann
...

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ASTM F2908-23(Specification)
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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 Compliance Audits to ASTM Standards on Unmanned Aircraft Systems

SIGNIFICANCE AND USE
4.1 The purpose of this standard practice is to provide the minimum requirements for the conduct of compliance audits.  
4.2 The intended use of this practice is to provide a basis for an internal or external entity to develop an audit program. An audit program defines specific requirements for the execution of audits for a particular objective. An example of an audit program would be an external (third party) audit of UAS manufacturer’s quality assurance system.  
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4.2 Successful completion of this training course neither constitutes nor implies certification or licensure from the CAA.  
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1.1 This specification defines the design, construction, and test requirements for a small unmanned aircraft system (sUAS).  
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ASTM F3423/F3423M-22(Specification)
Standard Specification for Vertiport Design

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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.  
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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.  
1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the D...

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