Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-445-3716 A 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. The assembled item forms a complete circle.
Alternate Parts: 4084743CLR, 4084743, 2840-01-445-3716, 01-445-3716, 2840014453716, 014453716
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 30, 1997 | 01-445-3716 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-445-3716
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084743CLR | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084743 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-445-3716
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 4.689 INCHES MINIMUM AND 4.714 INCHES MAXIMUM |
| SPECIAL FEATURES | DRAWING NAME VANE,TURBINE STATOR,3 STAGE,ASSY OF; OVERALL LENGTH IS FLOW AREA OF NOZZLE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100PW100 |