Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-433-5307 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: 9995M22G072A, 9995M22G07-2A, 9995M22G062A, 9995M22G06-2A, 2840-01-433-5307, 01-433-5307, 2840014335307, 014335307
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 02, 1996 | 01-433-5307 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-433-5307
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9995M22G07-2A | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| 9995M22G06-2A | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
Technical Data | NSN 2840-01-433-5307
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| SPECIAL FEATURES | DUAL ROTORS; HIGH BYPASS FAN |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$ACZCJ |
| END ITEM IDENTIFICATION | F108 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |