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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRPLANE STRENGTH AND RIGIDITY, LANDING AND GROUND HANDLING LOADS
23-07-2013
English
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Superseded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 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-A-8868 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
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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