MIL-DTL-87218E

CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL

contributor author	DLA - GS5 - DLA Aviation - Richmond
date accessioned	2017-09-04T18:00:31Z
date available	2017-09-04T18:00:31Z
date copyright	09/27/2012
date issued	2012
identifier other	FWWKZEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9F/handle/yse/183552
description abstract	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.Intended Use: The lockclad control cable assemblies and lockclad material covered by this specification are intended for use in aircraft control cable systems where low elongation under tension loads and/or a coefficient of thermal expansion more nearly matching that of a basically aluminum airframe is desired or required. Where these factors are not significant, unclad wire rope per MIL-DTL-83420 may be used for avoidance of the weight penalty of lockclad.
language	English
title	MIL-DTL-87218E	num
title	CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL	en
type	standard
page	15
status	Active
tree	DLA - GS5 - DLA Aviation - Richmond:;2012
contenttype	fulltext