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MIL A 008862 : A

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

Available format(s)

PDF

Language(s)

English

Superseded date

23-07-2013

€16.67
Excluding VAT

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Superseded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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€16.67
Excluding VAT