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National Stock Number:
3040-00-781-0255
Federal Supply Class:
3040
National Item Identification Number:
007810255
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).
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Manufacturer Information:
| 114C3340-7 | 77272 | THE BOEING COMPANY | | 114C3340-7 | 81205 | THE BOEING COMPANY |
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Techincal Specification:
| END ATTACHMENT HOLE DIAMETER | 0.250 INCHES NOMINAL BOTH ENDS | | END ATTACHMENT LENGTH | 2.280 INCHES NOMINAL FIRST END | | END ATTACHMENT LENGTH | 2.380 INCHES NOMINAL SECOND END | | END ATTACHMENT WIDTH | 0.500 INCHES NOMINAL SECOND END | | END ATTACHMENT WIDTH | 0.437 INCHES NOMINAL FIRST END | | BODY CONSTRUCTION | TUBULAR | | BODY DIAMETER | 0.625 INCHES NOMINAL | | LINK STYLE | SOLID SHANK | | OVERALL LENGTH | 16.820 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-6736, COND H, T-125 MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | STEEL | | SPECIAL FEATURES | EFFECTIVE LENGTH: 15.880 INCHES; LINK THREAD INFO: LENGTH 15.880 INCHES, RIGHT HAND, 3/8-24 UNF, DIAMETER 0.800 INCH 1ST END, 1.080 INCHES 2ND END, MATERIAL STEEL BOTH ENDS, SURFACE TREATMENT CADMIUM PLATED BOTH ENDS, LOCKNUT, USED ON FUSELAGE SECTION OF AN AIRCRAFT |
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