NPFC - MIL-A-8860
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR
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| Organization: | NPFC |
| Publication Date: | 31 March 1971 |
| Status: | inactive |
| Page Count: | 15 |
scope:
This specification contains general requirements, which, in combination with other applicable specifications; define the structural design, analysis, laboratory test, and documentation requirements for airplanes. These requirements apply to all airplane airframe structures which are required to sustain loads under takeoff, flight, landing, ground handling, and laboratory test conditions.
intended Use:
This specification is to be used for the structural design and structural substantiation of airplanes.
Document History
June 24, 2019
Airplane Strength and Rigidity, General Specification for
A description is not available for this item.
May 20, 1987
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR
This specification contains general requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing...
May 18, 1987
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-A-8860
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR
This specification contains general requirements, which, in combination with other applicable specifications; define the structural design, analysis, laboratory test, and documentation requirements...
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR
General.-
This specification contains general requirements, which, in combination with other applicable specifications, define the structural design, analysis, test , and data requirements for fixed...