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NPFC - MIL-A-8862

AIRPLANE STRENGTH AND RIGIDITY-LANDPLANE LANDING AND GROUND HANDLING LOADS

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Organization: NPFC
Publication Date: 18 May 1960
Status: inactive
Page Count: 22

Document History

MIL-A-8862
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY-LANDPLANE LANDING AND GROUND HANDLING LOADS
The requirements of this specification are intended to be used for the structural design and structural substantiation of airplanes.
MIL-A-8862
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY-LANDPLANE LANDING AND GROUND HANDLING LOADS
A description is not available for this item.

References

This document references:
MIL-A-8860 - Airplane Strength and Rigidity, General Specification for
Published by NPFC on June 24, 2019
A description is not available for this item.
This document references:
MIL-A-8867 - Airplane Strength and Rigidity Ground Tests
Published by NPFC on July 9, 2019
A description is not available for this item.
This document references:
MIL-T-6053 - TESTS, IMPACT, SHOCK ABSORBER LANDING GEAR, AIRCRAFT
Published by NPFC on July 20, 1977
This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data...
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