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Development and Qualification of Composite Landing Gears
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STANDARD published on 1.9.2020
Designation standards: SAE AIR5552
Publication date standards: 1.9.2020
SKU: NS-1004995
Country: American technical standard
Category: Technical standards SAE
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).
SUBJECT TAXONOMY: Landing gear, Braking systems, Air brakes, Tires and traction, On-board diagnostics (OBD), Maintainability and supportability, Parts, Bearings, Safety, Tests and Testing
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
Latest update: 2024-03-25 (Number of items: 2 885 931)
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