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Historical

SAE AIR5552

Development and Qualification of Composite Landing Gears

Standard by SAE International, 2020-09-17

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  • Language: English
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About This Item

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.
SKU: 1679cb3ad809

  • Publication Date: 2020-09-17
  • Standard Status: historical
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Nanomaterials, Commercial aircraft, Landing gear, Materials properties, Composite materials, Metals, Coatings, colorants, and finishes, Finite element analysis, Fatigue
  • Official SAE: Doi link
  • New Version Available: AIR5552A (2025-09-23)
  • This Version: AIR5552 (2020-09-17)

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