Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-908-6982 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: 65C34190CL9, 65C34192CL9, 65C34190CL9, 389451CL9, 348351CL9, 2840-00-908-6982, 00-908-6982, 2840009086982, 009086982
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-908-6982 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-908-6982
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 65C34190CL9 | 98750 | SAN ANTONIO AIR LOGISTICS CENTER |
| 65C34192CL9 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 65C34190CL9 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 389451CL9 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 348351CL9 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-908-6982
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| SPECIAL FEATURES | T.O. 2J-J57-54; NOZZLE ASSY; INCLUDES STAGES 2-3; 1.286-1.294 SQ. IN. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |