Historical

SAE AIR1494A

Name: SAE AIR1494A PDF | Request Standard
SKU: 38a732f2e9fb

Verification of Landing Gear Design Strength

Standard by SAE International, 2007-07-09

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Language: English

License Type: Single User

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SAE AIR1494A

AIR1494A.pdf

About This Item

Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear. An industry survey was recently conducted to determine just what analysis and testing are currently being applied to landing gear. Timing in relation to first flight of new aircraft was also questioned. Opinions were solicited from designers of the following categories and/or types of aircraft: a Military - Large Land Based (Bomber) b Military - Small Land Based (Fighter) c Military - Carrier Based (Navy) d Military - Helicopter (Large) e Military - Helicopter (Small-attack) f Commercial - Large (Airliner) g Commercial - Small (Business) h USAF (WPAFB) - Recommendations It is the objective of this AIR to present a summary of these responses. It is hoped that this summary will be useful to designers as a guide and/or check list in establishing criteria for landing gear analysis and test. This document has been reaffirmed to comply with the SAE 5-Year Review policy.

SKU: 38a732f2e9fb

Publication Date: 2007-07-09

Standard Status: historical

Publisher: SAE International

Document Type: Aerospace Standard

Subject: Failure modes and effects analysis, Commercial aircraft, Business and general aviation aircraft, , , , , ,

Official SAE: Doi link

New Version Available: AIR1494B (2010-04-13)
This Version: AIR1494A (2007-07-09)
Previous Version: AIR1494 (1978-02-01)

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SAE AIR1494A

Verification of Landing Gear Design Strength

SAE AIR1494A

About This Item

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