Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-394-5225 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: 804351CL16, 804351CL16, 804341, 2840-01-394-5225, 01-394-5225, 2840013945225, 013945225
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 09, 1994 | 01-394-5225 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-394-5225
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 804351CL16 | 96965 | TURBINE AIRFOIL DESIGNS INC. |
| 804351CL16 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 804341 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-394-5225
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 4.980 INCHES MINIMUM AND 5.030 INCHES MAXIMUM |
| SPECIAL FEATURES | FLOW AREA IS 1.409 MIN. TO 1.418 MAX. DIAMETER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR,1 STG |