Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-354-6143 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: 6082T04G02, 2840-01-354-6143, 01-354-6143, 2840013546143, 013546143
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 02, 1992 | 01-354-6143 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-354-6143
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6082T04G02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-354-6143
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | A1$$A2 |
| END ITEM IDENTIFICATION | T700-GE-401C ENGINE MODEL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MATCHED ASSY HIGH PRESSURE TURBINE LOW STRESS ROTOR |