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About This Item

 

Full Description

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.
 

Document History

  1. MIL MIL-DTL-87218E

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    Cable, Lockclad, for Aircraft Control

    • Most Recent
  2. MIL MIL-DTL-87218D


    CABLE, LOCKCLAD, FIR AIRCRAFT CONTROL (SUPERSEDING MIL-DTL-87218C)

    • Historical Version
  3. MIL MIL-DTL-87218C


    CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL (SUPERSEDING MIL-DTL-87218B) (S/S BY MIL-DTL-87218D)

    • Historical Version
  4. MIL MIL-DTL-87218B


    CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL (SUPERSEDING MIL-DTL-87218A) (S/S BY MIL-DTL-87218C)

    • Historical Version
  5. MIL MIL-DTL-87218A


    CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL (SUPERSEDING MIL-C-87218) (S/S BY MIL-DTL-87218B)

    • Historical Version
 

Amendments, rulings, supplements, and errata

  1. MIL MIL-DTL-87218E Notice 1 - Validation 1


    Cable, Lockclad, for Aircraft Control