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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Formerly under the jurisdiction of Committee F38 on Unmanned Aircraft Systems, this practice was withdrawn in July 2016 in accordance with section 10.5.3.1 of the Regulations Governing ASTM Technical Committees, which requires that standards shall be updated by the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.
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.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
F2279 Practice for Quality Assurance in the Manufacture of Fixed Wing Light Sport Aircraft
FAA Standards14 CFR Part 43 Maintenance, Preventive Maintenance, Rebuilding and Alteration
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ASTM F2512-07, Standard Practice for Quality Assurance in the Manufacture of Light Unmanned Aircraft System (Withdrawn 2016), ASTM International, West Conshohocken, PA, 2007, www.astm.orgBack to Top