WIRE ROPE, FLEXIBLE, CORROSION-RESISTING, NONMAGNETIC, FOR AIRCRAFT CONTROL

Amended by

MIL-DTL-18375H:2005/NOTICE 2:2020

Available format(s)

PDF

Published date

04-01-2005

Publisher

US Military Specs/Standards/Handbooks

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES

Describes the requirements for nonmagnetic, corrosion-resistant steel wire rope used in aircraft flight controls.

Committee	FSC 1640
DevelopmentNote	Supersedes MIL W 18375 (B) (10/2003) H NOTICE 1 - Notice of Validation. (01/2015) NEW CHILD NOT 2 2020 IS ADDED
DocumentType	Standard
Pages	33
ProductNote	NEW CHILD NOT 2 2020 IS ADDED
PublisherName	US Military Specs/Standards/Handbooks
Status	Current
Supersedes	MIL W 18375 : B MIL DTL 18375 : G

SAE AS 94900 : 2007	AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-DTL-6117 Revision L:2008	WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE
MIL-DTL-9490 Revision E:2008	FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

MIL-STD-129 Revision R:2014	Military Marking for Shipment and Storage
MIL-DTL-781 Revision J:2014	TERMINAL, WIRE ROPE SWAGING, GENERAL SPECIFICATION FOR
ASTM A 342/A342M : 2014 : REDLINE	Standard Test Methods for Permeability of Weakly Magnetic Materials
ASTM E 8/E8M : 2016-09	TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS

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Abstract