Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-430-0435 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: 9547M18G10, 2840-01-430-0435, 01-430-0435, 2840014300435, 014300435
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 23, 1996 | 01-430-0435 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-430-0435
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9547M18G10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-430-0435
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F110-14, FIG 75; REWKD & REIDENTIFED FROM 9547M18G08 |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | F110-129 AIRCRAFT GAS TURBINE ENGINE |