Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-122-1879 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: 23004362, 23004362, 2840-01-122-1879, 01-122-1879, 2840011221879, 011221879
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 15, 1981 | 01-122-1879 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-122-1879
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23004362 | 73342 | ALLISON TRANSMISSION, INC. |
| 23004362 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-122-1879
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 14.590 INCHES NOMINAL |
| DIAMETER | 16.000 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF41 |
