MIL A 8862 : 0
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS
English
12-07-1974
Gives the strength and rigidity requirements for field-landing and ground-handling loads of land-based and carrier-based airplanes applicable to procurement of airplanes.
| Committee |
FSC 1510
|
| DevelopmentNote |
Document has been cancelled but informs you to use MIL-A-8863.
|
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-L-87139 Base Document:1979 | LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL-A-8871 Revision A:1971 | Airplane Strength and Rigidity Flight and Ground Operations Tests (for Future Procure. (see MIL-A-87221) |
| SAE ARP1311C | Landing Gear Structures and Mechanisms |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| MIL-B-8584 Revision C:1970 | Brake Systems, Wheel, Aircraft, Design of |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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