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SAE AIR5552

Development and Qualification of Composite Landing Gears
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SAE AIR5552

Development and Qualification of Composite Landing Gears

PUBLISH DATE 2010
PAGES 16
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This information report provides general guidance for the design considerations, qualification in endurance, strength and fatigue of landing gear using composite components as principle structural elements. The information discussed herein includes the development and evaluation of design data considering: the potential for imbedded manufacturing defects, manufacturing process variations, the component operating environment, potential damage threats in service, rework and overhaul, and inspection processes. This AIR mainly discusses the use of thick composites for landing gear structural components. Considerations and recommendations provided in this AIR may therefore differ greatly from considerations and recommendations found in widely accepted composite design references such as CMH-17 and Advisory Circulars such as AC 20-107(B).
SDO SAE: SAE International
Document Number AIR5552
Publication Date Oct. 7, 2010
Language en - English
Page Count 16
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Oct. 7, 2010 AIR5552 Revision