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NPFC - MIL-A-8861

AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS

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Organization: NPFC
Publication Date: 5 December 1994
Status: active
Page Count: 1

Document History

July 9, 2019
Airplane Strength and Rigidity Flight Loads
A description is not available for this item.
MIL-A-8861
December 5, 1994
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
A description is not available for this item.
March 7, 1986
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
A description is not available for this item.
February 7, 1986
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
The requirements of this specification are intended to be used for the structural design of airplanes as affected by inflight loads.
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
This specification contains the strength and rigidity requirements for flight loading conditions applicable to airplanes.
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
This specification contains the strength and rigidity requirements for flight loading conditions applicable to procurement of airplanes.

References

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