| Name | Support | Language | Availability | Edition date | Price | ||
|---|---|---|---|---|---|---|---|
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PDF |
English |
Active |
7/14/2020 |
€116.00 |
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Details
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.
Additional Info
| Author | Society of Automotive Engineers International (SAE) |
|---|---|
| Committee | A-5B Gears, Struts and Couplings Committee |
| Published by | SAE |
| Document type | Standard |
| ICS | 49.045 : Structure and structure elements
|
| Number of pages | 24 |
| Replace | SAE ARP 5644:2019-04-17 |
| Document history | SAE ARP 5644:2019-04-17 |
| Keyword | SAE 5644,SAE ARP5644A,SAE ARP5644A,SAE ARP 5644 |
