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ASTM F2512-07

(Practice)

Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016)

Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016)

SIGNIFICANCE AND USE
The purpose of this practice is to provide the minimum requirements necessary for the establishment of a quality assurance and production acceptance program for a manufacturer of light airplane UAS.
SCOPE
1.1 This practice establishes the minimum requirements for the development of a Quality Assurance and Production Acceptance Program, to be used for the manufacture of Light Airplane Unmanned Aircraft Systems (UAS).
1.2 Other documents relevant to this practice include Practice F 2279, 14 CFR Part 21, 14 CFR Part 23, and 14 CFR Part 43.
1.3 This standard does not purport to address the quality assurance of the data-links, autopilot functions, and control stations.
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 and health practices and determine the applicability of regulatory limitations prior to use.
WITHDRAWN RATIONALE
This practice established the minimum requirements for the development of a Quality Assurance and Production Acceptance Program, to be used for the manufacture of Light Airplane Unmanned Aircraft Systems (UAS).
Formerly under the jurisdiction of Committee F38 on Unmanned Aircraft Systems, this practice was withdrawn in July 2016 in accordance with section 10.5.3.1 of the Regulations Governing ASTM Technical Committees, which requires that standards shall be updated by the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Withdrawn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-Apr-2007
Withdrawal Date
10-Jul-2016
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F38 - Unmanned Aircraft Systems
Drafting Committee
F38.01 - Airworthiness
Current Stage
Ref Project

Relations

Referred By
ASTM F3060-20 - Standard Terminology for Aircraft
Effective Date
15-Apr-2007

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ASTM F2512-07 - Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016)ASTM F2512-07 - Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016)
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ASTM F2512-07 - Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016)
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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: F2512 − 07
StandardPractice for
Quality Assurance in the Manufacture of Light Unmanned
1
Aircraft System
This standard is issued under the fixed designation F2512; 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 3.1.1 airplane, n—engine-driven fixed-wing aircraft heavier
than air, that is supported in flight by the dynamic reaction of
1.1 This practice establishes the minimum requirements for
the air against its wings.
the development of a Quality Assurance and Production
3.1.2 light airplane UAS, n—light airplane unmanned air-
Acceptance Program, to be used for the manufacture of Light
craft system; maximum gross weight 1320 lb.
Airplane Unmanned Aircraft Systems (UAS).
3.1.3 manufacturer, n—any entity engaged in the production
1.2 Other documents relevant to this practice include Prac-
of an unmanned aircraft system.
tice F2279, 14 CFR Part 21, 14 CFR Part 23, and 14 CFR Part
43.
3.1.4 permanent record, n—records shall be kept for each
light airplane UAS produced.
1.3 This standard does not purport to address the quality
assurance of the data-links, autopilot functions, and control 3.1.5 pilot operating handbook (POH), n—developedbythe
stations. airplane manufacturer and contains FAA-approved airplane
flight manual information.
1.4 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the 3.1.6 quality assurance manual (QAM), n—documentation
responsibility of the user of this standard to establish appro- of the quality assurance program.
priate safety and health practices and determine the applica-
3.1.7 quality assurance program (QAP), n—method of in-
bility of regulatory limitations prior to use.
spections used by the manufacturer to verify and ensure the
proper production thereof.
2. Referenced Documents
3.1.8 quality assurance record (QAR), n—record of quality
2
2.1 ASTM Standards:
assurance associated with each light airplane UAS produced.
F2279 Practice for QualityAssurance in the Manufacture of
3.2 Acronyms:
Fixed Wing Light Sport Aircraft
3 3.2.1 AOI, n—aircraft operating instructions
2.2 FAA Standards:
3.2.2 MRB, n—materials review board
14 CFR Part 21 Certification Procedures for Products and
Parts
3.2.3 UAS, n—unmanned aircraft system
14 CFR Part 23 Airworthiness Standards
14 CFR Part 43 Maintenance, Preventive Maintenance, Re- 4. Significance and Use
building and Alteration
4.1 The purpose of this practice is to provide the minimum
requirements necessary for the establishment of a quality
3. Terminology
assurance and production acceptance program for a manufac-
3.1 Definitions:
turer of light airplane UAS.
5. Quality Assurance Program (QAP)
1
This practice is under the jurisdiction ofASTM Committee F38 on Unmanned
Aircraft Systems and is the direct responsibility of Subcommittee F38.01 on
5.1 Manufacturers of light airplane UAS shall develop a
Airworthiness.
Quality Assurance Program (QAP) in accordance with the
Current edition approved April 15, 2007. Published May 2007. DOI: 10.1520/
criteria established within this practice.
F2512-07.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
5.2 Quality Assurance Manual (QAM)—Each manufacturer
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
shall document their QAP in the form of a Quality Assurance
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. Manual (QAM).
3
AvailablefromU.S.GovernmentPrintingOfficeSuperintendentofDocuments,
5.3 Quality Assurance Administration—The manufacturer’s
732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, http://
www.access.gpo.gov. administration that is charged with the implementation of the
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F2512 − 07
QAP may consist of one or more: company employees, duction of airframe components considered by the manufac-
company officials, or manufacturer’s agents or assigns. The turertobecriticaltothestructuralintegrityofthelightairplane
individual’s that make up the quality assurance administration UAS, such as welding, brazing, heat treatment, plating, struc-
shall be identified within the QAM. tural composites, adhesive bonding, and so forth, that ensures
that each process and service is performed in accordance with
5.4 Quality Assurance Record (QAR)—A record shall be
approved specifications containing definitive standards of
maintained of the date of acceptance, the o
...

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