NPFC - MIL-A-8861
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
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| Organization: | NPFC |
| Publication Date: | 31 March 1971 |
| Status: | inactive |
| Page Count: | 24 |
scope:
This specification contains the strength and rigidity requirements for flight loading conditions applicable to airplanes.
intended Use:
The requirements of this specification are intended for the structural design and structural substantiation of airplanes.
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.
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.
MIL-A-8861
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.