I
iwL-A-88683(As)
20 May 1987
SUPERSEDING
ML-A-8868A
8 February 1974
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MILITARY SPECIFICATION
AIRPLANE STRENGTH AND RIGIDITY
DATA AND REPORTS
This spec~ficatlon 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 Oefense.
1.
SCOPE
1.1 scope.
This speclf~cation contains the requirements for data
necessary to show compliance with the design and test requirements of 141L-A-
~
8860 th%uah l’41L-A-8870for the acaulsltion of naval afrplanes, and to show the
dependent ~elatlonshlp bet~een the-schedules for structural engineering
analyses and testing and schedules for manufacturing.
2. APPLICABLE DOCUMENTS
2.1 Government documents.
2.1.1 Specifications, standards, and handbooks.
The following
speciflcatlons,standards, and handbooks form a part of this specification to
the extent specified herein.
Unless otherwise specified, the Issues of these
documents shall be those Ilsted in the issue of the Department of Defense Index
of Specifications
solicitation.
SPECIFICATIONS
MILITARY
Oal-r)-?ooo
hlIL-L-8552
hlIL-o-870’8
MIL-A-8860
and Standards (DODISS) and supplement thereto, cited in the
Orawing, Engineer~ng and Associated List.
Landing Gear, Aircraft Shock Absorber (Air-Oil Type).
Demonstration Requirements for Airplanes.
Afrplane Strength and Rtgidity, General Specifications for.
~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 using the self-addressed
Standardization Oocument Improvement Proposal (00 Form 14261 appearing at the
end Of this document or by letter.
I
AMSC
FSC 1510
DISTRIBUTION STATEMENTA. Approved for public release; distribution is unlimited.
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