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NPFC - MIL-DTL-83420

WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR

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Organization: NPFC
Publication Date: 1 April 2005
Status: inactive
Page Count: 26
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 °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.

Document History

January 23, 2017
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
March 1, 2016
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
January 4, 2011
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
February 17, 2009
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
MIL-DTL-83420
April 1, 2005
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
November 20, 2002
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
November 5, 2001
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
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...
December 21, 2000
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. The wire rope, type I should be capable of operation within a −54 °C to...
October 30, 1999
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. The wire rope, Type I should be capable of operation within a −54° C to...
February 22, 1999
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. The wire rope, Type I should be capable of operation within a −54° C to...
August 15, 1997
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. The wire rope, Type I should be capable of operation within a −54°C to...
June 6, 1994
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. The wire rope, Type I shall be capable of operation within a −54°C to +...
October 30, 1987
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
January 18, 1985
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
February 14, 1984
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
April 25, 1983
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion-resistant steel wire rope used in aircraft flight controls. The wire rope, type I shall be capable of operation within a -54°...
March 31, 1982
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
July 25, 1979
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
April 29, 1977
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
November 12, 1976
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
A description is not available for this item.
September 7, 1973
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
This specification covers the requirements for carbon steel and corrosion-resistant steel wire rope used in aircraft flight controls, The wire rope, bare or nylon-jacketed, shall be capable of...

References

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