Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-436-7055 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: 6037T83P04, 2840-01-436-7055, 01-436-7055, 2840014367055, 014367055
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 25, 1996 | 01-436-7055 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-436-7055
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6037T83P04 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-436-7055
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 10 |
| OVERALL LENGTH | 5.246 INCHES MINIMUM AND 5.257 INCHES MAXIMUM |
| DIAMETER | 11.825 INCHES MINIMUM AND 11.835 INCHES MAXIMUM |
| SPECIAL FEATURES | BLADES ARE DOVETAILED; MATL SPEC INCONEL 718 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF-34-100A ACFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL,COMPRESSOR ROTOR |