Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-353-8342 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: 6082T04G05, 2840-01-353-8342, 01-353-8342, 2840013538342, 013538342
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 18, 1992 | 01-353-8342 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-353-8342
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6082T04G05 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-353-8342
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| END ITEM IDENTIFICATION | ITEM USED ON TURBO PROP ENGINES (T700) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MATCHED ASSY HIGH PRESSURE TURBINE LOW STRESS ROTOR |