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Landing Gear Shock Absorption Testing of Civil Aircraft
- Aerospace Standard
Published July 14, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
The report is revised to: (1) update references for Part 23 aircraft, (2) add a section on unique Russian requirements, (3) update section on gas absorption testing, (4) add equation for drop height, (5) update all equations for latest version of Word, and (6) include other minor updates and corrections.
Data Sets - Support Documents
|Table 1||Summary of Part 25 main gear drop test conditions|
|14CFRPART23||This document is not part of the subscrption.|
|14CFRPART25||This document is not part of the subscrption.|
|14CFRPART29||This document is not part of the subscrption.|
|CS-23||This document is not part of the subscrption.|
|CS-25||This document is not part of the subscrption.|
|CS-27||This document is not part of the subscrption.|
|CS-29||This document is not part of the subscrption.|
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