Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-224-2201 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: 37D401329G022, 2840-01-224-2201, 01-224-2201, 2840012242201, 012242201
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 14, 1986 | 01-224-2201 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-224-2201
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37D401329G022 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-224-2201
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. J-85/-17 |