Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-304-3018 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: 1359M35P01110, 1359M35P01-110, 1359M35, 2840-01-304-3018, 01-304-3018, 2840013043018, 013043018
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 15, 1989 | 01-304-3018 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-304-3018
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1359M35P01-110 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| 1359M35 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
Technical Data | NSN 2840-01-304-3018
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 52, IND 25 |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |