Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-212-9006 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: 9550M19G02, 2840-01-212-9006, 01-212-9006, 2840012129006, 012129006
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 19, 1985 | 01-212-9006 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-212-9006
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9550M19G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-212-9006
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-F101-4, FIG 1, IND 19; INCLUDES 1ST & 2ND STG DISKS |
| END ITEM IDENTIFICATION | F101 AIRCRAFT ENGINE |