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Landing Gear Shock Absorption Testing of Civil Aircraft
- Aerospace Standard
Published April 17, 2019 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.
This SAE Aerospace Recommended Practice (ARP) has been developed to document the requirements for jig drop testing of civil aircraft landing gear. It details the requirements of the FAA Code of Federal Regulations and EASA Certification Specifications. It provides recommendations for drop test procedures, data collection, test conditions, post-test inspections, and test reporting. It also provides guidance for analytical test correlation.
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.|