Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-475-0260 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: 9995M23G032A, 9995M23G03-2A, 9995M23G012A, 9995M23G01-2A, 9995M23G082A, 9995M23G08-2A, 9995M23G062A, 9995M23G06-2A, 2840-01-475-0260, 01-475-0260, 2840014750260, 014750260
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 18, 2000 | 01-475-0260 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-475-0260
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9995M23G03-2A | 58828 | CFM INTERNATIONAL, INC. |
| 9995M23G01-2A | 58828 | CFM INTERNATIONAL, INC. |
| 9995M23G08-2A | 58828 | CFM INTERNATIONAL, INC. |
| 9995M23G06-2A | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 2840-01-475-0260
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 36.000 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F108-4 |
| END ITEM IDENTIFICATION | F108-CF-100 |