Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-448-6985 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 4084517705, 4084517-705, 4084517700, 4084517-700, 4084517, 4083015701, 4083015-701, 2840-01-448-6985, 01-448-6985, 2840014486985, 014486985
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-6985 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-6985
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084517-705 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084517-700 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084517 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4083015-701 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-6985
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 1; LOCATION NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT; USE ONLY ON P/N 4084522-800, -801, -802 AND 4082657-808 |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR AND STATOR ASSY, TURBINE REAR COMPRESSOR DRIVE |