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SAE AIR5914

Current Revision

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.

SDO SAE: SAE International
Document Number AIR5914
Publication Date June 10, 2014
Language en - English
Page Count 18
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
June 10, 2014 AIR5914 Revision