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NAVY - MIL-A-8867

AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS

inactive
Organization: NAVY
Publication Date: 18 May 1960
Status: inactive
Page Count: 26
scope:

General.- This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes. The types of testing include, but are not limited to:

(a) Static tests.

(b) Drop tests of structurally complete airframes,

(c) Elevated temperature tests,

(d) Repeated load tests. Cabin pressure tests,

(e) Cabin pressure tests,

(f) Leakages tests of integral fuel tanks.

intended Use:

The requirements of this specification shall be used for the structural substantiation of airplanes.

Document History

July 9, 2019
Airplane Strength and Rigidity Ground Tests
A description is not available for this item.
October 3, 1994
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
A description is not available for this item.
March 25, 1993
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
A description is not available for this item.
June 10, 1987
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes....
May 18, 1987
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
A description is not available for this item.
August 22, 1975
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
A description is not available for this item.
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
A description is not available for this item.
MIL-A-8867
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
General.- This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted...

References

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