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SAE ARP 5644:2019-04-17

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SAE ARP 5644:2019-04-17

Landing Gear Shock Absorption Testing of Civil Aircraft

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The intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.
Author SAE
Editor SAE
Document type Standard
Format File
Confirmation date 2019-04-17
ICS 49.045 : Structure and structure elements
Number of pages 24
Set AEROPAKS10U-10
Year 2019
Document history
Country USA
Keyword SAE 5644;SAE ARP5644;SAE ARP5644;SAE ARP 5644