Full Description

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: 07/14/2020 Number of Pages: 24 File Size: 1 file , 480 KB Redline File Size: 2 files , 4.4 MB