INCH-POUND
MIL-DTL-18375H
1 April 2005
SUPERSEDING
MIL-DTL-18375G
5 November 2001
DETAIL SPECIFICATION
WIRE ROPE, FLEXIBLE, CORROSION-RESISTING,
NONMAGNETIC, FOR AIRCRAFT CONTROL
This specification is approved for use by all Departments and Agencies of the
Department of Defense.
1. SCOPE
1.1 Scope. This specification covers the requirements for nonmagnetic, corrosion-
resistant steel wire rope used in aircraft flight controls. The wire rope will be capable of
operation within a -65 °F to +250 °F (-54 °C to +121 °C) temperature range in wind, dust, fuel
and oil spills, in aircraft wash-down and other environmental stresses and aircraft experiences.
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3 and 4 of
this specification. This section does not include documents cited in other sections of this
specification or recommended for additional information or as examples. While every effort has
been made to ensure the completeness of this list, document users are cautioned that they must
meet all specified requirements of the documents cited in sections 3 and 4 of this specification,
whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications and standards. The following specification and standard form a part
of this document to the extent specified herein. Unless otherwise specified, the issues of these
documents are those cited in the solicitation or contract.
Comments, suggestions, or questions on this document should be addressed to Defense Supply
Center Richmond, ATTN: DSCR-VEB, 8000 Jefferson Davis Highway, Richmond, VA 23297-
5616 or emailed to STDZMGT@dla.mil. Since contact information can change, you may want
to verify the currency of this address information using the ASSIST database at
AMSC N/A
FSC 1640
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