Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-006-3028 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: 717103, 2840-01-006-3028, 01-006-3028, 2840010063028, 010063028
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 15, 1975 | 01-006-3028 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-006-3028
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 717103 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
Technical Data | NSN 2840-01-006-3028
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 1.610 INCHES MINIMUM AND 1.614 INCHES MAXIMUM |
| DIAMETER | 9.769 INCHES MINIMUM AND 9.777 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,MODEL NO. J69T25 |