3040-14-322-0234

Rigid Connecting Link

3040143220234 143220234 0000481151 481151

An item of various cross-sectional shapes which may be of solid or hollow construction. It is specifically designed for attachment to a lever(s) and/or control(s) to actuate various remote mechanisms. It is one of the following: (1) A one-piece item with or without eyes and/or holes in each end which may have bushings or bearings pressed in the eyes; (2) A one-piece item with both ends processed for terminations, excluding threaded end(s); (3) A two-piece construction type item consisting of a body with both ends processed for terminations and a single end attachment; or (4) A three-piece construction type item consisting of a body and two end attachments. Excludes internal combustion engine type piston connecting rods; DRAG LINK, STEERING; LINK, ANCHOR, BRAKE SHOE; TIE ROD, STEERING; and TURNBUCKLE. For cylindrical shaped externally threaded items without end attachments, see ROD, THREADED END and STUD (as modified). View more Rigid Connecting Link

3040-14-322-0234 CONNECTING LINK,RIGID 3040143220234 143220234

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
3040-14-322-0234 CONNECTING LINK,RIGID 3040143220234 143220234 1/1
NSN 3040-14-322-0234 (Generic Image) 1/1

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3040-14-322-0234 Related Documents Related Documents 3040-14-322-0234 5+ Documents (More...)

2840-00-754-4824 2840007544824 007544824 is a single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
2840-00-754-4825 2840007544825 007544825 is a single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
2840-00-754-4826 2840007544826 007544826 is a single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
5970-99-628-2758 5970996282758 996282758 is a rigid or flexible tubing having other than uniform fabricated shapes or forms. it is specifically designed to prevent any undesirable flow of current between conductors or between conductors and other objects. includes shrinkable type items. excludes items not having rated electrical characteristics. also excludes bushing, sleeve; cable nipple, electrical; and insulation sleeving, electrical.
2840-00-754-4828 2840007544828 007544828 is a single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.

3040-14-322-0234 Demil Restrictions 3040-14-322-0234

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

3040-14-322-0234 is a Rigid Connecting Link

3040-14-322-0234 End Users End Users 3040-14-322-0234

France (ZF)

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