Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-394-7115 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: 804351CL22, 804351CL22, 804351CL22, 804351, 2840-01-394-7115, 01-394-7115, 2840013947115, 013947115
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 12, 1994 | 01-394-7115 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-394-7115
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 804351CL22 | 99160 | THERM, INCORPORATED |
| 804351CL22 | 96965 | TURBINE AIRFOIL DESIGNS INC. |
| 804351CL22 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 804351 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-394-7115
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| OVERALL WIDTH | 2.045 INCHES NOMINAL |
| OVERALL HEIGHT | 4.153 INCHES NOMINAL |
| SPECIAL FEATURES | FLOW AREA 1.464 - 1.489.PITCH IS 34DEG 38MIN 28SEC |
| CRITICALITY CODE JUSTIFICATION | ABMK |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31, IND 50 |
| END ITEM IDENTIFICATION | TF-33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT, 1 STG |