SAE AIR1494A PDF | Request Standard
Historical

SAE AIR1494A

Verification of Landing Gear Design Strength

Standard by SAE International, 2007-07-09

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  • Availability: Immediate Download
  • Language: English
  • License Type: Single User
  • Updates: Not Included
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  • Language: English
  • License Type: Enterprise / Multi User
  • Updates: Included

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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