Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-416-1723 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: 9550M19G26, 2840-01-416-1723, 01-416-1723, 2840014161723, 014161723
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 14, 1995 | 01-416-1723 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-416-1723
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9550M19G26 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-416-1723
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-F101-4, FIG 1, IND 19; INCLUDES STG 2 DISKS |
| END ITEM IDENTIFICATION | F101 AFCT GAS TURBINE ENGINE |