MIL A 008862 : A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AIRPLANE STRENGTH AND RIGIDITY, LANDING AND GROUND HANDLING LOADS
English
23-07-2013
Gives the strength and rigidity requirements for landing and ground-handling loads of airplanes.
| Committee |
FSC 1510
|
| DevelopmentNote |
Use this document in lieu of MIL-A-8862 (1960).
|
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-T-6053 Revision C:1977 | Tests, Impact, Shock Absorber Landing Gear, Aircraft |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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