Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-323-9769 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: 4076770, 4076770, 2840-01-323-9769, 01-323-9769, 2840013239769, 013239769
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 06, 1990 | 01-323-9769 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-323-9769
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4076770 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4076770 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-323-9769
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 3.140 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F100-54; STATORS RUN COUNTERCLOCKWISE; MATL IS COBALT |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ACFT ENG |