1680-00-824-2084 SEAT,AIRCRAFT Index 2810-00-824-2086 SUPPORT ASSEMBLY

National Stock Number:
3040-00-824-2085

Federal Supply Class:
3040

National Item Identification Number:
008242085

Description:
CONNECTING LINK,RIGID

Detail:
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).


Manufacturer Information:
114C3010-177272THE BOEING COMPANY
114C3010-181205THE BOEING COMPANY


Techincal Specification:
END ATTACHMENT HOLE DIAMETER0.312 INCHES NOMINAL BOTH ENDS
END ATTACHMENT LENGTH2.577 INCHES NOMINAL FIRST END
END ATTACHMENT LENGTH3.115 INCHES NOMINAL SECOND END
END ATTACHMENT WIDTH0.437 INCHES NOMINAL FIRST END
END ATTACHMENT WIDTH0.687 INCHES NOMINAL SECOND END
BODY CONSTRUCTIONTUBULAR
BODY DIAMETER1.750 INCHES NOMINAL
LINK STYLESOLID SHANK
OVERALL LENGTH34.470 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONWW-T-785, TY-1, T4 - CANCELED FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY
SPECIAL FEATURESEFFECTIVE LENGTH: 33.250 INCHES; LINK THREAD INFO: LENGTH 1.250 INCHES, RIGHT HAND, 1/2-20 OR 3/8-24 NF; END ATTACHMENT INFO: DIAMETER 1.031 INCHES 1ST END, 1.410 INCHES 2ND END, MATERIAL CORROSION RESISTANT STEEL 1ST END, STEEL 2ND END, SURFACE TREATMENT PASSIVATED 1ST END, CADMIUM PLATED 1ST END, LOCKNUT, USED ON AIRCRAFT FUSELAGE SECTION


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