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Crashworthy Landing Gear Design
- Aerospace Standard
Published November 09, 2015 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear.
This document covers the field of commercial and military airplanes and helicopters. This summary of crashworthy landing gear design requirements and approaches may be used as a reference for future aircraft.
AIR4566A has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Aircraft Indicating Systems|
|Aerospace Standard||Aircraft Nosewheel Steering/Centering Systems|
|Aerospace Standard||Design and Verification of Aircraft Nose Wheel Steering Systems|
Data Sets - Support Documents
|TABLE 1||SIKORSKY CRASHWORTHY LANDING GEARS|
|14 CFR 23.561, 23.721, 25.561, 25.721, 27.561, 29.561||This document is not part of the subscrption.|
|14CFR23.561,23.||This document is not part of the subscrption.|
|AFSCDH2-1||This document is not part of the subscrption.|
|CS 23.561, 23.721, 25.561, 25.721, 27,561, 29.561||This document is not part of the subscrption.|
|CS23.561,23.721||This document is not part of the subscrption.|
|MIL-STD-1290||This document is not part of the subscrption.|
|SD-24L||This document is not part of the subscrption.|
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