Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK AND HUB
2840-01-460-4380 An item that consists of a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE and a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 983525230, 9835252-30, 2840-01-460-4380, 01-460-4380, 2840014604380, 014604380
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 04, 1998 | 01-460-4380 | 50565 ( DISK AND HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-460-4380
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9835252-30 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-460-4380
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O.2J-TF33-34 FIG. 5B, INDEX 1A,HUB AND BLADE ASSEMBLY FRONT COMPRESSOR, NOTE: USED ON TF33-102C, 1ST STAGE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33-102C |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DISK AND BLADE ASSEMBLY 1ST STAGECOMPRESSOR |