NPFC - MIL-A-8866
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
active, Most Current
Buy Now
| Organization: | NPFC |
| Publication Date: | 20 May 1987 |
| Status: | active |
| Page Count: | 15 |
scope:
This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.
intended Use:
The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
Document History
July 9, 2019
Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance
A description is not available for this item.
October 3, 1994
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
A description is not available for this item.
May 20, 1987
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
This specification defines the strength and rigidity requirement for repeated loading condition applicable to Navy procured airplanes.
MIL-A-8866
May 20, 1987
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.
May 18, 1987
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
A description is not available for this item.
August 22, 1975
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
This specification identifies the durability design requirements applicable to the structure of airplanes. The complete structure, here in referred to as to as the airframe, includes the fuselage,...
January 21, 1974
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
A description is not available for this item.
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
The requirements of this specification are intended to be used for the structural design and substantiation of airplanes.
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
This specification contains the reliability oriteria and repeated loads spectra applicable to procurement of airplanes
Related Products
Searching for related products...