NPFC - MIL-A-8861
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
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| Organization: | NPFC |
| Publication Date: | 7 February 1986 |
| Status: | active |
| Page Count: | 34 |
scope:
This specification covers the requirements for strength and rigidity for flight loading conditions applicable to airplanes.
intended Use:
The requirements of this specification are intended to be used for the structural design of airplanes as affected by inflight loads.
Document History
July 9, 2019
Airplane Strength and Rigidity Flight Loads
A description is not available for this item.
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.
MIL-A-8861
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.
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