Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-447-4909 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: 4084243CLM, 4084243, 2840-01-447-4909, 01-447-4909, 2840014474909, 014474909
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 07, 1997 | 01-447-4909 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-4909
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084243CLM | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084243 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-447-4909
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.820 INCHES NOMINAL |
| OVERALL WIDTH | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM |
| OVERALL HEIGHT | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 109; FLOW AREA 4.615-4.639 SQUARE INCH AREA |
| CRITICALITY CODE JUSTIFICATION | AMATT$$AABKW$$AABMK$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-100/200/220E AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE,TURBINE STATOR |