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ASTM F3003-14

(Specification)

Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)

Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)

ABSTRACT
This specification establishes the quality assurance requirements for the design, manufacture, and production of a small unmanned aircraft system (sUAS). It is intended for all sUAS that are permitted to operate over a defined area and in airspace defined 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
1.1 This standard defines the quality assurance requirements for the design, manufacture, and production of a small unmanned aircraft system (sUAS).  
1.2 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 and health practices and determine the applicability of regulatory limitations prior to use.
WITHDRAWN RATIONALE
This standard defines the quality assurance requirements for the design, manufacture, and production of a small unmanned aircraft system (sUAS).
Formerly under the jurisdiction of Committee F38 on Unmanned Aircraft Systems, this specification was withdrawn in January 2023 in accordance with Section 10.6.3 of the Regulations Governing ASTM Technical Committees, which requires that standards shall be updated by the end of the eighth year since the last approval date.

General Information

Status
Withdrawn
Publication Date
14-Jan-2014
Withdrawal Date
08-Jan-2023
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F38 - Unmanned Aircraft Systems
Drafting Committee
F38.01 - Airworthiness
Current Stage
Ref Project

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ASTM F3003-14 - Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)ASTM F3003-14 - Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)
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ASTM F3003-14 - Standard Specification for Quality Assurance of a Small Unmanned Aircraft System (sUAS) (Withdrawn 2023)
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation:F3003 −14
Standard Specification for
Quality Assurance of a Small Unmanned Aircraft System
1
(sUAS)
This standard is issued under the fixed designation F3003; 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 3.1.5 quality assurance program, QAP, n—method of in-
spections used by the manufacturer to validate and ensure the
1.1 This standard defines the quality assurance requirements
proper production thereof.
for the design, manufacture, and production of a small un-
manned aircraft system (sUAS). 3.1.6 quality assurance record, QAR, n—record of quality
assurance associated with each sUAS produced.
1.2 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
3.1.7 small unmanned aircraft system, sUAS, n—composed
responsibility of the user of this standard to establish appro- ofthesmallunmannedaircraft(sUA)andallrequiredon-board
priate safety and health practices and determine the applica-
subsystems, payload, control station, other required off-board
bility of regulatory limitations prior to use. subsystems, any required launch and recovery equipment, and
command and control (C2) links between the UA and the
2. Referenced Documents
control station. For purposes of this standard, sUAS is synony-
2
2.1 ASTM Standards:
mous with a small Remotely Piloted Aircraft System (sRPAS)
F2910 Specification for Design, Construction, and Test of a andsUAissynonymouswithasmallRemotelyPilotedAircraft
Small Unmanned Aircraft System (sUAS)
(sRPA).
3.1.8 supplier, n—any entity engaged in the design and
3. Terminology
production of components (other than a payload which is not
3.1 Definitions of Terms Specific to This Standard:
required for safe operation of the sUAS) used on a sUAS.
3.1.1 manufacturer, n—entity responsible for assembly and
3.1.8.1 Discussion—Where the supplier is not the
integration of components and subsystems to create a safe
manufacturer, the supplier can only ensure that the components
operating sUAS. The builder of kit built systems provided by
comply with accepted consensus standards.
a manufacturer must conform to the manufacturer’s assembly
3.2 Shall versus Should versus May—Use of the word
and test instructions without deviation in order for that kit built
“shall” implies that a procedure or statement is mandatory and
system to meet this standard.
must be followed to comply with this standard, “should”
3.1.2 permanent record, n—records that shall be kept for
implies recommended, and “may” implies optional at the
each sUAS produced.
discretion of the supplier, manufacturer, or operator. Since
3.1.3 propulsion system, n—consists of one or more power
“shall” statements are requirements, they include sufficient
plants (for example, a combustion engine or an electric motor
detail needed to define compliance (for example, threshold
and, if used, a propeller or rotor) together with the associated
values, test methods, oversight, reference to other standards).
installation of fuel system, control and electrical power supply
“Should” statement are provided as guidance towards the
(for example, batteries, electronic speed controls, fuel cells, or
overall goal of improving safety, and could include only
other energy supply).
subjective statements. “Should” statements also represent pa-
3.1.4 quality assurance manual, QAM, n—documentation
rameters that could be used in safety evaluations, and could
of the quality assurance program.
lead to development of future requirements. “May” statements
are provided to clarify acceptability of a specific item or
1 practice, and offer options for satisfying requirements.
This test method is under the jurisdiction of ASTM Committee F38 on
UnmannedAircraftSystemsandisthedirectresponsibilityofSubcommitteeF38.01
on Airworthiness.
4. Applicability
Current edition approved Jan. 15, 2014. Published January 2014. DOI: 10.1520/
F3003-14.
4.1 This standard is written for all sUAS that are permitted
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
to operate over a defined area and in airspace defined by a
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
nation’sgoverningaviationauthority(GAA).Itisassumedthat
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. a visual observer(s) will provide for the sense-and-avoid
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3003−14
requirement to preve
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