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MIL-A-8863B(AS)
6 May 1987
SUPERSEDING
MIL-A-8863A
12 July 1974
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MILITARY SPECIFICATION
AIRPLANE STRENGTH
AND RIGIDITY
GROUND LOADS
FOR NAVY ACQUIRED AIRPLANES
This specification IS approved
for use within the Naval Air
Systems
Command, Department of the Navy, and is available
for use by all Departments and Agencies of the Department
of Defense.
1.
SCOPE
1.1 Scope.
This specification defines the strength and rigidity
requirements
for ground load~ng conditions applicable to Navy acquired
airplanes.
2.
APPLICABLE DOCUMENTS
2.1 Government documents.
2.1.1 Specfficatlons and Standards.
The following specifications and
standards form a part of this specification to the extent
specified herein.
Unless otherwise specified, the Issues of these documents shall be those
llsted fn the Issue of the Department of Defense
Index of Specifications and
Standards (0001SS), and supplement thereto, ctted in the solicitation.
SPECIFICATIONS
MIL-D-8708 -
Demonstration Requirements for Airplanes.
HIL-A-8860 -
Airplane Strength and Rigidity, General
Specification for.
MIL-A-8867 - Airplane Strength
and Rlgldlty Ground Tests.
Beneficial comments (recommendations, additions, deletions) and any pertinent
data which may be of use tn Improving this document should be addressed to:
Naval Air Engineering Center, Systems Englneerlncjand Standardization
Department (Code 93), Lakehurst,
NJ 08733-5100, by using the self-addressed
Standardization Document Improvement Proposal {DO Form 1426) appearing at the
end of this document, or by letter.
AMSC hilA
FSC
1510
DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
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