NSN 3040-00-824-2085
Part Details | RIGID CONNECTING LINK
3040-00-824-2085 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: 114C30101, 114C3010-1, 114C30101, 114C3010-1, 3040-00-824-2085, 00-824-2085, 3040008242085, 008242085
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | JAN 01, 1960 | 00-824-2085 | 21988 ( CONNECTING LINK, RIGID ) |
REFERENCE DRAWINGS & PICTURES
ANGLED
Cross Reference | NSN 3040-00-824-2085
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114C3010-1 | 81205 | THE BOEING COMPANYDBA BOEING |
| 114C3010-1 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 3040-00-824-2085
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | WW-T-785, TY-1, T4 - CANCELED FED SPEC SINGLE MATERIAL RESPONSE |
| BODY CONSTRUCTION | TUBULAR |
| LINK STYLE | 4 ANGLED |
| OVERALL LENGTH | 34.470 INCHES NOMINAL |
| BODY DIAMETER | 1.750 INCHES NOMINAL |
| SPECIAL FEATURES | EFFECTIVE LENGTH: 33.250 INCHES; LINK THREAD INFO: LENGTH 1.250 INCHES, RIGHT HAND, 1/2-20 OR 3/8-24 NF; END ATTACHMENT INFO: DIAMETER 1.031 INCHES 1ST END, 1.410 INCHES 2ND END, MATERIAL CORROSION RESISTANT STEEL 1ST END, STEEL 2ND END, SURFACE TREATMENT PASSIVATED 1ST END, CADMIUM PLATED 1ST END, LOCKNUT, USED ON AIRCRAFT FUSELAGE SECTION |