Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-499-0449 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: 5111T23G08, 2840-01-499-0449, 01-499-0449, 2840014990449, 014990449
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 11, 2002 | 01-499-0449 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-499-0449
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5111T23G08 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-499-0449
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | GE F414-400 ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ROTOR ASSY, HIGH PRESSURE TURBINE F414 |