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MIL-A-8861 Revision B:1986

Current

Current

The latest, up-to-date edition.

AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS

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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES

Describes requirements for strength and rigidity for flight loading conditions.

Committee
FSC 1510
DevelopmentNote
Supersedes MIL A 008861 (A). (07/2005)
DocumentType
Standard
Pages
33
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

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SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-HDBK-1763 Base Document:1998 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
MIL-A-8871 Revision A:1971 AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES

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-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

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