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: 53G9706017, 53G970601-7, 53G97060117, 53G970601-17, 53G970601, 3040-00-005-7279, 00-005-7279, 3040000057279, 000057279
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | JUN 16, 1972 | 00-005-7279 | 21988 ( CONNECTING LINK, RIGID ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT
Cross Reference | NSN 3040-00-005-7279
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 53G970601-7 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 53G970601-17 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 53G970601 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 3040-00-005-7279
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| BODY CONSTRUCTION | SOLID |
| LINK STYLE | STRAIGHT |
| OVERALL LENGTH | 1.920 INCHES NOMINAL |
| BODY WIDTH | 0.920 INCHES NOMINAL |
| BODY THICKNESS | 0.327 INCHES NOMINAL |
| SPECIAL FEATURES | CONNECTING 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 IDENTIFICATION | AIRCRAFT F-4 & F-5, NEXT HIGHER ASSY-OUTER WING SLAT MECHANISM |
