Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-447-2505 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: 9547M14G08, 9547M14, 2840-01-447-2505, 01-447-2505, 2840014472505, 014472505
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 30, 1997 | 01-447-2505 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2505
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9547M14G08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9547M14 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2505
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM |
| SPECIAL FEATURES | INCLUDES STAGES 1-9; HPCR STG 1-2 HAS IMPROVED SPOOL OIL DRAIN HOLES (2) THAT ARE 1.48 TIME LARGER THAN THE CURRENT ELLIPTICAL HOLE; REPLACES P/N 9547M14G03 AND 9547M14G06; CHANGE OF HOLE IS A PHYSICAL CHANGE BUT NOT FUNCTIONALLY INTERCHANGEABLE |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ$$AABHP |
| END ITEM IDENTIFICATION | F110-129 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR |