Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-064-3140 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: 6893556, 6893556, 2840-01-064-3140, 01-064-3140, 2840010643140, 010643140
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 22, 1978 | 01-064-3140 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-064-3140
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6893556 | 73342 | ALLISON TRANSMISSION, INC. |
| 6893556 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-064-3140
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE MODEL TF41 |