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
