NSN 1680-00-540-3448
Part Details | FLEXIBLE SHAFT ASSEMBLY
1680-00-540-3448 An item consisting of a casing with fittings and attachments on each end and a spirally wound wire core with formed end(s) and/or crimped on end fittings. It is designed to transmit rotary motion around bends from a motor or other power source to drive various types of equipment, such as tachometers, speedometers, remote controls, instruments, and the like, which are located at an angle and/or distance from the power source. See also CONTROL ASSEMBLY, PUSH-PULL.
Alternate Parts: 3155601100, 31556-011-00, 3155601100, 31556-011-00, 1680-00-540-3448, 00-540-3448, 1680005403448, 005403448
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 01, 1963 | 00-540-3448 | 20315 ( SHAFT ASSEMBLY, FLEXIBLE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-00-540-3448
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 31556-011-00 | 35351 | GE AVIATION SYSTEMS LLC |
| 31556-011-00 | 31435 | LUCAS AEROSPACE POWER EQUIPMENTCORPORATION |
Technical Data | NSN 1680-00-540-3448
| Characteristic | Specifications |
|---|---|
| CASING MATERIAL | STEEL, CORROSION RESISTING |
| CASING LENGTH BETWEEN FERRULES | 11.000 INCHES NOMINAL |
| CASING OUTSIDE DIAMETER | 0.544 INCHES MINIMUM AND 0.560 INCHES MAXIMUM |
| CORE MATERIAL | STEEL |
| CORE OVERALL LENGTH | 11.9062 INCHES NOMINAL |
| CORE DIAMETER | 0.307 INCHES MINIMUM AND 0.317 INCHES MAXIMUM |
| CORE ROTATION DIRECTION | C$D |
| CORE REMOVABILITY | NONREMOVABLE |
| OVERALL LENGTH | 11.9062 INCHES NOMINAL |
| TORSIONAL DEFLECTION RATING | 1.2 FT-LB IN. TORSIONAL DEFLECTION RATING IN WINDING DIRECTION,2.0 FT-LB IN. IN UNWINDING DIRECTION |
| MINIMUM OPERATING RADIUS | 20.000 INCHES |
| FSC APPLICATION DATA | FLAP ACTUATING SYSTEM INSTALLATION AIRCRAFT |