Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-443-4068 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: 1385M24P05118, 1385M24P05-118, 2840-01-443-4068, 01-443-4068, 2840014434068, 014434068
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 09, 1997 | 01-443-4068 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-4068
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1385M24P05-118 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-443-4068
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | SAME AS P/N 1385M24P05 BUT ONLY TO BE USED ON THE F118 ENGINE |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |