Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-323-5919 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: 4077094, 4077094, 2840-01-323-5919, 01-323-5919, 2840013235919, 013235919
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 31, 1990 | 01-323-5919 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-323-5919
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4077094 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4077094 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-323-5919
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 3.140 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| DIAMETER | 2.480 INCHES NOMINAL |
| SPECIAL FEATURES | NOZZLE STATOR IS COUNTERCLOCKWISE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |