MIL-DTL-18375H: 2005
Current
The latest, up-to-date edition.
WIRE ROPE, FLEXIBLE, CORROSION-RESISTING, NONMAGNETIC, FOR AIRCRAFT CONTROL
01-04-2005
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 AS94900 | 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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