درباره ما
MIL-DTL-83420M (2)
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
| contributor author | DLA - GS5 - DLA Aviation - Richmond | |
| date accessioned | 2017-09-04T17:48:52Z | |
| date available | 2017-09-04T17:48:52Z | |
| date copyright | 01/04/2011 | |
| date issued | 2011 | |
| identifier other | ESGOIDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=authoCA58ear3081D20686159DD6EFDEC014A/handle/yse/172034 | |
| description abstract | 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 °F to +250 °F (-54 °C to +121 °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 °F to +200 °F (-54 °C to +94 °C) temperature range in wind, dust, fuel, and oil spills, in wash-down and other environmental stresses and aircraft experiences.Intended Use: The wire rope covered by this specification is intended for use in aircraft flight control systems applications where high resistance is needed against corrosion, abrasion, and fatigue wear. | |
| language | English | |
| title | MIL-DTL-83420M (2) | num |
| title | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR | en |
| type | standard | |
| page | 26 | |
| status | Active | |
| tree | DLA - GS5 - DLA Aviation - Richmond:;2011 | |
| contenttype | fulltext | |
| subject keywords | Airplane | |
| subject keywords | Coated | |
| subject keywords | Guide | |
| subject keywords | Plated | |
| subject keywords | Pliable | |
| subject keywords | Steel cable | |
| subject keywords | Uncoated |
