Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-123-1045 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: 6009T42P05, 2840-01-123-1045, 01-123-1045, 2840011231045, 011231045
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 05, 1981 | 01-123-1045 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-123-1045
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6009T42P05 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-123-1045
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL-CENTRIFUGAL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 5.895 INCHES MINIMUM AND 5.899 INCHES MAXIMUM |
| DIAMETER | 13.064 INCHES MINIMUM AND 13.072 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME SPOOL,AXIAL COMPRESSOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ROTOR SPOOL,REAR-COMPRESSOR |