Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-476-6468 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: 815967, 2840-01-476-6468, 01-476-6468, 2840014766468, 014766468
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 18, 2000 | 01-476-6468 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-476-6468
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 815967 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2840-01-476-6468
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 48.000 INCHES NOMINAL |
| DIAMETER | 40.000 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| SUPPLEMENTARY FEATURES | SHAFT, DISC, AND BLADES |
| REFERENCE DATA AND LITERATURE | 2J-TF33-34 |
| END ITEM IDENTIFICATION | TF33 ENGINE |