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This specification covers the minimum requirements for production acceptance testing of a powered parachute aircraft. The test includes ground and flight testing. In ground testing, the aircraft shall undergo inspection verification and engine break-in. In flight testing, on the other hand, the aircraft shall be inspected for performance while on a specified flight time, including takeoff and landing, and shall undergo instrument verification. In addition, this specification also provides for post flight acceptance testing, which shall include a review of all flight critical attachments and structures.
This abstract is a brief summary of the referenced standard. It is informational only and not an official part of the standard; the full text of the standard itself must be referred to for its use and application. ASTM does not give any warranty express or implied or make any representation that the contents of this abstract are accurate, complete or up to date.
ICS Number Code 49.020 (Aircraft and space vehicles in general)
UNSPSC Code 25132005(Ultra light aircraft)
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ASTM F2242-05(2013), Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft, ASTM International, West Conshohocken, PA, 2013, www.astm.orgBack to Top