NSN 1680-01-015-2606
Part Details | AIRCRAFT EJECTION SEAT
1680-01-015-2606 A seat designed to be ejected through an aircraft canopy or hatch opening, by means of some form of an explosive.
Alternate Parts: 59418183, 5941818-3, 21821151115, 218-21151-115, 1680-01-015-2606, 01-015-2606, 1680010152606, 010152606
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 16, 1976 | 01-015-2606 | 20316 ( SEAT, AIRCRAFT EJECTION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1680-01-015-2606
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5941818-3 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 218-21151-115 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 1680-01-015-2606
| Characteristic | Specifications |
|---|---|
| EJECTION DIRECTION | UPWARD |
| PARACHUTE FOR WHICH DESIGNED | BACK |
| EJECTION CONTROL LOCATION | LEFT ARM REST |
| ADJUSTABILITY | ADJUSTABLE |
| SWIVEL | NOT INCLUDED |
| ARMREST | INCLUDED |
| ADJUSTMENT TYPE | VERTICAL |
| PERSONAL EQUIPMENT ACCOMMODATION | C ANY ACCEPTABLE |
| OVERALL LENGTH | 36.000 INCHES NOMINAL |
| OVERALL WIDTH | 17.740 INCHES NOMINAL |
| OVERALL HEIGHT | 46.950 INCHES NOMINAL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |