Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-475-3393 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 1359M16G06110B, 1359M16G06-110B, 2840-01-475-3393, 01-475-3393, 2840014753393, 014753393
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 31, 2000 | 01-475-3393 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-475-3393
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1359M16G06-110B | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-475-3393
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| OVERALL LENGTH | 14.500 INCHES NOMINAL |
| DIAMETER | 17.000 INCHES NOMINAL |
| SPECIAL FEATURES | SUPPORTS STAGE 4-9 BLADES,PROVIDEDS SEAL TEETH TO PREVENT AIR RECIRCULATION UNDER STAGES 4-9 VANE SHROUD AND TRANSMITS TORQUE BETWEEN THE HPT SHAFTAND HPC FRONT SHAFT |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110-100B 2J-F100-4 |