Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-212-2127 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: 6006T80G30, 2840-01-212-2127, 01-212-2127, 2840012122127, 012122127
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 08, 1985 | 01-212-2127 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-212-2127
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6006T80G30 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-212-2127
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| DIAMETER | 16.706 INCHES MINIMUM AND 16.720 INCHES MAXIMUM |
| SPECIAL FEATURES | WAS COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| REFERENCE DATA AND LITERATURE | 2J-J85-54 |
| END ITEM IDENTIFICATION | ACFT ENG J85-GE-21B |