Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-448-3147 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: 9550M14G06, 2840-01-448-3147, 01-448-3147, 2840014483147, 014483147
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 26, 1997 | 01-448-3147 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-3147
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9550M14G06 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-448-3147
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 28.000 INCHES NOMINAL |
| DIAMETER | 25.000 INCHES NOMINAL |
| SPECIAL FEATURES | FRACTURE CRITICAL ITEM; STGS 1 AND 2 SPOOL; FORWARD STUB-SHAFT; STG 3 DISK; REAR ROTATING AIR SEAL; T.O. 2J-F118-3-1 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABMZ$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F101-GE-102 AIRCRAFT GAS TURBINE ENGINE |