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Development and Qualification of Composite Landing Gears
- Aerospace Standard
- AIR5552
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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).
Rationale
AIR5552 has been reaffirmed to comply with the SAE five-year review policy.
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Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
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Issuing Committee
Reference
Number | Title |
---|---|
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 - AIRCRAFT |
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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