Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-443-2713 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: 5101T32G01, 2840-01-443-2713, 01-443-2713, 2840014432713, 014432713
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 07, 1997 | 01-443-2713 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-2713
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5101T32G01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-443-2713
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | A1-F414A-IPB-400,FIGURE 047/INDEX 2 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | LOW PRESSURE TURBINE MODULE;F414-GE-400 ENGINE |