MIL-A-M61B(AS)
7 February 1986
SUPERSEDING
.*
7-
*
1.
rig
2.
MIL-A-8861(ASG)
18 May 1960
(See section 6.4)
MILITARY
SPECIFICATION
AIRPLANE STRENGTH AND RIGIDITY
FLIGHT LOADS
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.
SCOPE
1.1 Scope.
This speclficaton covers the requirements for strength and
dity for flight loading conditions applicable to airplanes.
APPLICABLE DOCUMENTS
2.1 Government documents.
2.1.1 Specifications.
The following specifications form a part of this
@
specification to the extent spectfied herein, Unless otherwise specified, the
issues of these documents shall be those listed in the Issue of the Department
of Defense Endex of Specifications and Standards (0001SS) and supplement
thereto, cited in the solicitation.
I
I
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 ard Standardization
Department, (Code 93), Lakehurst, NJ 08733-5100, by using the self-addressed
Standardization Document Improvement Proposal (OD Form 1426) appearing at the
end of this document or by letter.
AMSC N!A FSC 1510
DISTRIBUTION STATEMEPJTA.
Approved for public release; distribution is unlimited.
m
*
Downloaded from http://www.everyspec.com
