MIL-A-6865B(AS)
20 Nay 1987
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SUPERSEDING
MJL-A-8865(ASG)
18 May 1960
MILITARY SPECIFICATION
AIRPLANE STRENGTH ANO RIGIDITY MISCELLANEOUS LOAOS
This specification is approved for usd within the Naval Alr Systems
Command, Department of the Navy, and Is available for use by ail
Departments and Agencies of the Department of Defense.
1. SCOPE
1.1 we. This speclf~cation contains the strength and rigidity
requirements for miscellaneous load: applicable to acqui>ltlon of airplanes.
2. APPLICABLE DOCUMENTS
2. I Government documents.
2.1.1 Specifications.
The following specifications form a part of this
specification to the extent specified herein. Unless otherwise specified,
the issues of these documents shall be those iisted in the issue of the
Department of Defense Index of Specifications and Standards (0001SS) and
supplement thereto, cited in the solicitation.
SPECIFICATIONS
MILITARY
MIL-D-8708
Demonstration Requirements for Airplanes.
MIL-A-8867
Airplane Strength and Rigidity - Ground Tests
MIL-A-8868
Airpiane Strength and Rigidity - Data and
Reports.
(Copies of specifications required by contractors in connection with
specific acquisition functions shouid be obtained from the contracting
activity or as directed by the contracting activity. )
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Beneflclal comments (recommendations, additions, deletions) and any pertinent
data which may be of use in lmprovlng this document should be addressed to:
Systems Engineering and Standardization Department (Code 93), Naval Air
Engineering Center, Lakehurst, NJ 08733-5100, by using the self-addressed
Standardization Document Improvement Proposai (DD Form 1426) appearing at the
end of this document or by letter.
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AMSC NIA
DISTRIBUTION STATEMENT A
Approved for public release; distribu
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FSC i5i0
ion is unlimited.
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