Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-443-3148 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: 4083582, 2840-01-443-3148, 01-443-3148, 2840014433148, 014433148
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 07, 1997 | 01-443-3148 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-3148
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083582 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-443-3148
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 18; REPLACES P/NS 4072682, 4079932, 4079942, 4079192 AND 4080352 |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ$$ACZCJ |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE,TURBINE STATOR |