NSN 1680-01-073-2784
Part Details | AIRCRAFT EJECTION SEAT
1680-01-073-2784 A seat designed to be ejected through an aircraft canopy or hatch opening, by means of some form of an explosive.
Alternate Parts: J117202503, J117202-503, 22021151112, 220-21151-112, 1680-01-073-2784, 01-073-2784, 1680010732784, 010732784
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | MAR 13, 1979 | 01-073-2784 | 20316 ( SEAT, AIRCRAFT EJECTION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-01-073-2784
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| J117202-503 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 220-21151-112 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 1680-01-073-2784
| Characteristic | Specifications |
|---|---|
| EJECTION DIRECTION | UPWARD |
| PARACHUTE FOR WHICH DESIGNED | BACK |
| EJECTION CONTROL LOCATION | BELOW LEFT ARM REST |
| ADJUSTABILITY | ADJUSTABLE |
| SWIVEL | NOT INCLUDED |
| ARMREST | INCLUDED |
| ADJUSTMENT TYPE | VERTICAL |
| OVERALL WIDTH | 17.740 INCHES NOMINAL |
| OVERALL HEIGHT | 49.390 INCHES NOMINAL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |