MIL-A-8871 Revision A:1971
Superseded
View Superseded by
Airplane Strength and Rigidity Flight and Ground Operations Tests (for Future Procure. (see MIL-A-87221)
English
07-01-1971
07-23-2013
Covers flight test requirements for structural integrity flight and ground evaluation and demonstration of piloted airplanes.
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification covers the flight test requirements for the structural integrity flight and ground evaluation and demonstration of piloted airplanes.
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-A-8865 Revision B:1987 | Airplane Strength and Rigidity Miscellaneous Loads |
| MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8861 Revision B:1986 | Airplane Strength and Rigidity Flight Loads |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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