Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-483-0254 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: 214114045, 2-141-140-45, 2840-01-483-0254, 01-483-0254, 2840014830254, 014830254
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 13, 2001 | 01-483-0254 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-483-0254
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-141-140-45 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-483-0254
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | CH-46 TURBINE ENGINE,MARKING REQUIREMENTS PER MC9014,MARK |