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SAE AIR1494B

Name: SAE AIR1494B PDF | Request Standard
SKU: 4b41582f6a2e

Verification of Landing Gear Design Strength

Standard by SAE International, 2010-04-13

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Language: English

License Type: Single User

Updates: Not Included

SAE AIR1494B

AIR1494B.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. mililtary - 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); and 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. AIR 1494 Verification of Landing Gear Design Strength will be cancelled as the contents of this document were included in the latest update of ARP1311C Landing Gear Structures and Mechanisms.

SKU: 4b41582f6a2e

Publication Date: 2010-04-13

Standard Status: latest

Publisher: SAE International

Document Type: Aerospace Standard

Subject: Landing gear, Test procedures, , , , , , ,

Official SAE: Doi link

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

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SAE AIR1494B

Verification of Landing Gear Design Strength

SAE AIR1494B

About This Item

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