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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