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MIL-DTL-18375H: 2005

Current

Current

The latest, up-to-date edition.

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

Available format(s)

PDF

Published date

01-04-2005

€17.95
Excluding VAT

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

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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