Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-372-3063 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: 114704201, 114704-201, 2840-01-372-3063, 01-372-3063, 2840013723063, 013723063
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 05, 1993 | 01-372-3063 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-372-3063
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114704-201 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2840-01-372-3063
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | AN ITEM THAT IS DESIGNED TO RECEIVE THE LATENT ENERGY OF COMBUSTION GAS. THE ITEM CONSISTS OF A DISK OR DISKS |
| END ITEM IDENTIFICATION | UH-60 SERIES HELICOPTER |