NSN 1680-01-083-1058
Part Details | AIRCRAFT EJECTION SEAT
1680-01-083-1058 A seat designed to be ejected through an aircraft canopy or hatch opening, by means of some form of an explosive.
Alternate Parts: J117201501, J117201-501, 22021151111, 220-21151-111, 1680-01-083-1058, 01-083-1058, 1680010831058, 010831058
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | SEP 16, 1979 | 01-083-1058 | 20316 ( SEAT, AIRCRAFT EJECTION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-01-083-1058
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| J117201-501 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 220-21151-111 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 1680-01-083-1058
| 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 | VERTICAL |
| PERSONAL EQUIPMENT ACCOMMODATION | BZ ANY ACCEPTABLE AND D ANY ACCEPTABLE AND C ANY ACCEPTABLE |
| OVERALL LENGTH | 47.000 INCHES NOMINAL |
| OVERALL WIDTH | 18.500 INCHES NOMINAL |
| OVERALL HEIGHT | 28.500 INCHES NOMINAL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |