Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-160-6481 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 752880, 2840-01-160-6481, 01-160-6481, 2840011606481, 011606481
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 24, 1983 | 01-160-6481 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-160-6481
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 752880 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-160-6481
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | WAS COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O.2J-TF33-34, FIG31, IND 2 |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TURBINE ROTOR ASSY-FRONT COMPRESSOR DRIVE |