NSN 3040-00-005-7279

Part Details | RIGID CONNECTING LINK

3040-00-005-7279 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).

Alternate Parts: 53G97060117, 53G970601-17, 53G970601, 53G9706017, 53G970601-7, 3040-00-005-7279, 00-005-7279, 3040000057279, 000057279

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
30JUN 16, 197200-005-727921988 ( CONNECTING LINK, RIGID )
REFERENCE DRAWINGS & PICTURES

STRAIGHT

Cross Reference | NSN 3040-00-005-7279
Part Number Cage Code Manufacturer
53G970601-1776301BOEING COMPANY, THEDBA BOEING
53G97060176301BOEING COMPANY, THEDBA BOEING
53G970601-776301BOEING COMPANY, THEDBA BOEING
Technical Data | NSN 3040-00-005-7279
Characteristic Specifications
MATERIAL ALUMINUM ALLOY
BODY CONSTRUCTION SOLID
LINK STYLE STRAIGHT
OVERALL LENGTH1.920 INCHES NOMINAL
BODY WIDTH0.920 INCHES NOMINAL
BODY THICKNESS0.327 INCHES NOMINAL
SPECIAL FEATURESCONNECTING HOLE BEARING LOCATION BOTH ENDS, END RADIUS 0.460 IN NOMINAL, END ATTACHMENT NOT INCLUDED, DISTANCE FROM END TO HOLE CENTER 0.460 IN NOMINAL, HOLE DIAMETER 0.625 IN NOMINAL, EFFECTIVE LENGTH 1.000 IN NOMINAL, LOCKNUT NOT INCLUDED
END ITEM IDENTIFICATIONAIRCRAFT F-4 & F-5, NEXT HIGHER ASSY-OUTER WING SLAT MECHANISM