|
描述 |
标准 |
MIL-DTL-87218 |
涵盖范围 |
This specification covers the requirements for lockclad control cable material used in aircraft flight controls and aircraft control cable assemblies that include lockclad as a portion of the assembly. Lockclad is defined as the resulting material of swaging aluminum alloy tubing onto MIL-DTL-83420, type I, nonjacketed wire rope to the extent necessary to comply with the elongation and coefficient of thermal expansion properties specified herein. |
描述 |
Cable, Lockclad, for Aircraft Control |
分类归属 |
1640 |
文档状态 |
有效
|
文档日期 |
2012-09-27 |
审查日期 |
2017-09-26 |
文档类型 |
Detail Specification |
文档注释 |
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起草机构 |
GS |
编制机构 |
DLA Aviation - Richmond |
协调级别 |
Full |
陆军管理 |
Aviation and Missile Command |
海军管理 |
Naval Air Systems Command |
空军管理 |
Air Force Life Cycle Management Center - Cataloging and Product Support |
国防后勤局管理 |
DLA Aviation - Richmond |