MIL-DTL-83420 Revision P:2017
Current
The latest, up-to-date edition.
Wire Rope, Flexible, for Aircraft Control, General Specification for
English
23-01-2017
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope.
| DevelopmentNote |
Supersedes MIL W 83420 (E). (03/2016)
|
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. Type I wire rope will be capable of operation within a -65 degree F to +250 degree F (-54 degree C to +121 degree C) temperature range in wind, dust, fuel, and oil spills, in wash-down and other environmental stresses and aircraft experiences. Type II wire rope will be capable of operation within a -65 degree F to +200 degree F (-54 degree C to +94 degree C) temperature range in wind, dust, fuel, and oil spills, in wash-down and other environmental stresses and aircraft experiences.
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