MI1-T-85075A(AS)
31 December 1985
SUPERSEDING
MIL-T-85075(AS)
14 November 1977
MILITARY SPECIFICATION
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR
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 covers the tie down assemblies for use on
helicopter blades.
APPLICABLE DOCUMENTS
2.
2.1
Government documents.
2.1.1 Specifications, standards, and handbooks. The following
specifications, standards, and handbooks form a part of this specification to
the extend specified herein. Unless otherwise specified, the issues of these
documents shall be those listed in the issue of the Department of Defense
Index of Specifications and Standards (DoDISS) and supplement thereto, cited
in the solicitation.
SPECIFICATIONS
FEDERAL
QQ-C-320
Chromium Plating (Electrodeposited)
Nickel Plating (Electrodeposited)
QQ-N-290
QQ-P-416
Plating, Cadmium (Electrodeposited)
Silver Plating, Electrodeposited,
General Requirements
QQ-S-365
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 Document Improvement Proposal (DD Form 1426) appearing at
the end of this document. or by letter.
AMSC N/A
FSC 1730
Approved for public release; distribution is unlimited.
DISTRIBUTION STATEMENT A.
For Parts Inquires submit RFQ to Parts Hangar, Inc.
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