Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK AND HUB
2840-01-447-2868 An item that consists of a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 1559M63G04, 2840-01-447-2868, 01-447-2868, 2840014472868, 014472868
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 31, 1997 | 01-447-2868 | 50561 ( DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2868
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1559M63G04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2868
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
| DIAMETER | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O 2J-F110-14, FIG 67, IND 5; REPL P/N 1559M63G02; HPCR STG 1-2 SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL, COMPRESSOR ROTOR |