Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-084-6852 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: 5013T22G17, 2840-01-084-6852, 01-084-6852, 2840010846852, 010846852
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 23, 1979 | 01-084-6852 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-084-6852
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5013T22G17 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-084-6852
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | T.O. 2J-J85-94; INCLUDES DISKS,BLADES,HUBS & THE LIKE,LOCATED ON A TURBINE SHAFT |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85 |