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Development and Qualification of Composite Landing Gears
- Aerospace Standard
Published September 17, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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).
AIR5552 has been reaffirmed to comply with the SAE five-year review policy.
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|AC20-107B||This document is not part of the subscrption.|
|AC23-13A||This document is not part of the subscrption.|
|AC25-571-1B||This document is not part of the subscrption.|
|AFS-120-73-2||This document is not part of the subscrption.|
|AIR1494||VERIFICATION OF LANDING GEAR DESIGN STRENGTH|
|ARP1311||Landing Gear Structures and Mechanisms|
|ARP5644||Landing Gear Shock Absorption Testing of Civil Aircraft|
|ARP5914||This document is not part of the subscrption.|
|CMH-17-F||This document is not part of the subscrption.|
|DOT/FAA/AR-03/1||This document is not part of the subscrption.|
|DOT/FAA/AR-03/19||This document is not part of the subscrption.|
|MMPDS,version3||This document is not part of the subscrption.|
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