I
MIL-A-8866C(AS)
20 May 1987
SUPERSEDING
MIL-A-8866(ASG)
18 May 1960
(See 6.4)
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MILITARY SPECIFICATION
AIRPLANE STRENGTH AND RIGIOITY RELIABILITY
REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
This specification is approved for use within the Naval
Air Systems Command, Department of the Navy, and is
available for use by alI Departments and Agencies of the
Department of Defense.
1. SCOPE
1.1 Scope. This specification defines the strength and rigidity
requirements for repeated loading condition applicable to Navy procured
airplanes.
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2.
APPLICABLE DOCUMENTS ....””K...
2.1 Government documents.
2.1.1 Specifications and Standards: 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 listed in the issue of
the Department of Oefense Index of Specifications and Standards (DDDISS) and
supplement thereto, cited in the solicitation.
SPECIFICATIONS
MILITARY
HIL-D-B708 - Demonstration Requirements for Airplanes.
HIL-A-B860 - Airplane Strength and Rigidity, General
Specification for.
NIL-A-8861 - Airplane Strength and Rigidity F1ight Loads.
MIL-A-8863 - Airplane Strength and Rigldity Ground Loads for
Navy Procured Airplanes.
HIL-A-B867 -
Airplane Strength and Rigidity Ground Tests.
Beneficial comments (recommendations, additions, deletions) and any pertinent
data which may be of use in improving this document should be addressed to:
Naval Air Engineering Center, Systems Engineering and Standardization
Department (Code 93), Lakehurst. NJ 08733-5100, by usin9 the self-addressed
Standardization OocurnentImprovement Proposal (DD Form 1426) appearing at the
end of this document, or by letter.
AMSC N/A
FSC 1510
DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
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