Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-348-2311 A component of a ROTOR, COMPRESSOR, 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, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 822634, 698997, 2840-01-348-2311, 01-348-2311, 2840013482311, 013482311
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 06, 1991 | 01-348-2311 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-348-2311
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 822634 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 698997 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-348-2311
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 16.500 INCHES NOMINAL |
| DIAMETER | 18.802 INCHES MINIMUM AND 18.804 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |