Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-382-1296 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
Alternate Parts: 9550M20G14, 9550M20G13, 2840-01-382-1296, 01-382-1296, 2840013821296, 013821296
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 28, 1993 | 01-382-1296 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-382-1296
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9550M20G14 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9550M20G13 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-382-1296
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | NOZZLE ASSEMBLY, SHROUD, SEALS AND STATORS; T.O. 2J-F101-4, FIG 1, IND 15 |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-102 |