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AS8860A - Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications

Details
Document Number: AS8860A
Revision Number: A
Title
Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
Scope
This specification contains landing gear strength and rigidity requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes.
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