NSN 3040-01-453-2977
Part Details | RIGID CONNECTING LINK
3040-01-453-2977 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: C0140281, C014028-1, C0140281, C014028-1, C014028, 3036AS445, 3036AS445, 3036AS445, 3036AS445, 3036AS445, 3040-01-453-2977, 01-453-2977, 3040014532977, 014532977
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | FEB 25, 1998 | 01-453-2977 | 21988 ( CONNECTING LINK, RIGID ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT
Cross Reference | NSN 3040-01-453-2977
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| C014028-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
| C014028-1 | 8V613 | BOEING COMPANY, THEDBA BOEING |
| C014028 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 3036AS445 | 05DN8 | KLUNE INDUSTRIES, INC.DIV KLUNE INDUSTRIES |
| 3036AS445 | 32067 | MARVIN ENGINEERING CO., INC.DBA MARVIN GROUP, THE |
| 3036AS445 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 3036AS445 | 072E5 | RAYTHEON COMPANYDBA RAYTHEON |
| 3036AS445 | 09245 | SOLO ENTERPRISE CORP.DBA SOLO GOLF |
Technical Data | NSN 3040-01-453-2977
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-25043 AL 17-7PH ANNEALED FN 2D MIL SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | PASSIVATE |
| BODY CONSTRUCTION | SOLID |
| LINK STYLE | STRAIGHT |
| BODY WIDTH | 0.260 INCHES NOMINAL |
| BODY THICKNESS | 0.080 INCHES NOMINAL |
| SPECIAL FEATURES | WITH TWO END HOLES 0.126 IN. NOM. DIA.; USED ON BRU-33A/A |
| END ITEM IDENTIFICATION | AIRCRAFT, HORNET F/A-18 |