Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-010-5949 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: 119001003, 1-190-010-03, 2840-01-010-5949, 01-010-5949, 2840010105949, 010105949
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 02, 1975 | 01-010-5949 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-010-5949
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-190-010-03 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-010-5949
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 66 BLADES; 12.935 IN. MIN 12.937 IN. MAX OD |