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SAE AIR 5914:2014-06-10

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SAE AIR 5914:2014-06-10

Landing Gear Fatigue Spectrum Development For Part 25 Aircraft

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This SAE Aerospace Information Report (AIR) provides guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear. Many of the recommendations herein are generalizations based on data obtained from a wide range of landing gears. The aircraft manufacturer or the landing gear supplier is encouraged to use data more specific to their particular undercarriage whenever possible.
Author SAE
Editor SAE
Document type Standard
Format File
ICS 49.045 : Structure and structure elements
Number of pages 18
Set AEROPAKS10U-10
Year 2014
Document history
Country USA
Keyword SAE 5914;SAE AIR5914;SAE AIR5914;SAE AIR 5914