NSN 3040-01-057-2590
Part Details | RIGID CONNECTING LINK
3040-01-057-2590 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: 53G97060115, 53G970601-15, 53G9706013, 53G970601-3, 53G97060115, 53G970601-15, 53G97060115, 53G970601-15, 53G970601, G97060115, G970601-15, CS3040SR0702, CS3040-SR-0702, 3040-01-057-2590, 01-057-2590, 3040010572590, 010572590
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | MAR 09, 1978 | 01-057-2590 | 21988 ( CONNECTING LINK, RIGID ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT
Cross Reference | NSN 3040-01-057-2590
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 53G970601-15 | 4T683 | AERO TECHNOLOGY COMPANY |
| 53G970601-3 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 53G970601-15 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 53G970601-15 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 53G970601 | 76301 | BOEING COMPANY, THEDBA BOEING |
| G970601-15 | 76301 | BOEING COMPANY, THEDBA BOEING |
| CS3040-SR-0702 | 16236 | DLA LAND AND MARITIMEDBA ENGINEERING AND TECHNICAL |
Technical Data | NSN 3040-01-057-2590
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| SURFACE TREATMENT | ANODIZE |
| BODY CONSTRUCTION | SOLID |
| LINK STYLE | STRAIGHT |
| OVERALL LENGTH | 2.200 INCHES NOMINAL |
| BODY WIDTH | 0.920 INCHES NOMINAL |
| BODY THICKNESS | 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM |
| SPECIAL FEATURES | NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | AIRCRAFT F-4 & F-5 |