Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-146-9475 A component of a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9524M58P02, 9524M58P01, 9524M58, 2840-01-146-9475, 01-146-9475, 2840011469475, 011469475
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 08, 1983 | 01-146-9475 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-146-9475
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9524M58P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9524M58P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9524M58 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-146-9475
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| DIAMETER | 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG 56, IND 22 |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-100 AND F110-GE-100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |