NSN 1680-01-053-3529
Part Details | AIRCRAFT EJECTION SEAT
1680-01-053-3529 A seat designed to be ejected through an aircraft canopy or hatch opening, by means of some form of an explosive.
Alternate Parts: 5821726517, 5821726-517, 21821151118, 218-21151-118, 1680-01-053-3529, 01-053-3529, 1680010533529, 010533529
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 03, 1978 | 01-053-3529 | 20316 ( SEAT, AIRCRAFT EJECTION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-01-053-3529
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5821726-517 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 218-21151-118 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 1680-01-053-3529
| Characteristic | Specifications |
|---|---|
| EJECTION DIRECTION | UPWARD |
| PARACHUTE FOR WHICH DESIGNED | BACK |
| EJECTION CONTROL LOCATION | ABOVE HEAD REST AREA |
| ADJUSTABILITY | ADJUSTABLE |
| SWIVEL | NOT INCLUDED |
| ARMREST | NOT INCLUDED |
| ADJUSTMENT TYPE | HORIZONTAL AND VERTICAL |
| OVERALL WIDTH | 14.938 INCHES NOMINAL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |