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.
Product Details
- Published:
- 04/17/2019
- File Size:
- 1 file , 960 KB
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- This product is unavailable in Ukraine, Russia, Belarus
