Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-498-2784 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: 31070801, 3107080-1, 2840-01-498-2784, 01-498-2784, 2840014982784, 014982784
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 20, 2002 | 01-498-2784 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-498-2784
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3107080-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-498-2784
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| END ITEM IDENTIFICATION | GARRETT TPE331-10 FOR CASA 212 TRANSPORT AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ROTOR ASSY., FIRST STAGE TURBINE |