NSN 3040-01-491-0581
Part Details | RIGID CONNECTING LINK
3040-01-491-0581 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: 160D9201141, 160D920114-1, 160D920114, 160D9201141, 160D920114-1, 3040-01-491-0581, 01-491-0581, 3040014910581, 014910581
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | OCT 11, 2001 | 01-491-0581 | 21988 ( CONNECTING LINK, RIGID ) |
REFERENCE DRAWINGS & PICTURES
EYE ENDS
Cross Reference | NSN 3040-01-491-0581
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 160D920114-1 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 160D920114 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 160D920114-1 | 61174 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 3040-01-491-0581
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | PAINT |
| BODY CONSTRUCTION | SOLID |
| LINK STYLE | EYE ENDS |
| OVERALL LENGTH | 3.0600 INCHES NOMINAL |
| BODY WIDTH | 0.5000 INCHES NOMINAL |
| BODY THICKNESS | 0.2190 INCHES MINIMUM AND 0.2290 INCHES MAXIMUM |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | AIRCRAFT, THUNDERBOLT II, A-10; AIRCRAFT, F-16 |