Document ID:

MIL-DTL-83420       Scroll down to access document images

Overview

Title:  Wire Rope, Flexible, for Aircraft Control, General Specification for Scope:  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. Status:  Active Document Date:  07-JAN-2022         Next Review Due:  06-JAN-2027 FSC/Area:  1640 Doc Category:   Detail Specification   Qualification

Responsibilities

Lead Standardization Activity:  GS  DLA Aviation - Richmond     Preparing Activity: GS5  DLA Aviation - Richmond Coordination:  Full   Army Custodian:  AV   Combat Capabilities Development Command, Aviation and Missile Center   Navy Custodian:  AS   Naval Air Systems Command   Air Force Custodian:  11   Air Force Life Cycle Management Center - Aircraft Systems   DLA Custodian:  GS   DLA Aviation - Richmond

Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.

Revision History

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