Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-308-4145 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: 6055T26G07, 2840-01-308-4145, 01-308-4145, 2840013084145, 013084145
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 28, 1989 | 01-308-4145 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-308-4145
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6055T26G07 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-308-4145
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | DYNAMIC BALANCE ROTOR ASSEMBLY AT 1500 RPM MINIMUM |
| END ITEM IDENTIFICATION | T700-401C ENGINE |