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MIL-A-8863

Revision C, July 19, 1993

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AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES



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Description / Abstract:

The requirements of this specification are intended for use in the structural design and substantiation of airplanes. These requirements may be modified for specific models of airplanes by type or detail specifications, by flight test or demonstration requirements, and by other contractual documents.