Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-174-5736 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: 9945M27G01, 9945M27G01, 2840-01-174-5736, 01-174-5736, 2840011745736, 011745736
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 21, 1984 | 01-174-5736 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-174-5736
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9945M27G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9945M27G01 | 98912 | JET ENGINE TECHNOLOGY CORPORATION |
Technical Data | NSN 2840-01-174-5736
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 6.280 INCHES MINIMUM AND 6.320 INCHES MAXIMUM |
| DIAMETER | 14.980 INCHES MINIMUM AND 15.000 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME HUB,TURBINE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F101 |