Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-411-3346 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: 9550M58G20, 9550M58G19, 9550M58G18, 2840-01-411-3346, 01-411-3346, 2840014113346, 014113346
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 22, 1995 | 01-411-3346 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-411-3346
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9550M58G20 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9550M58G19 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9550M58G18 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-411-3346
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | USED ON HPT ROTOR REAR SHAFT DAMPER SLEEVE, PER NEW T.O. 2J-F101-590 |
| END ITEM IDENTIFICATION | ACFT ENG F101 |