Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-471-7748 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: 822666, 801239, 2840-01-471-7748, 01-471-7748, 2840014717748, 014717748
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 14, 2000 | 01-471-7748 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-471-7748
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 822666 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 801239 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-471-7748
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-TF33-14 FIGURE 19 INDEX 5A |
| END ITEM IDENTIFICATION | TF33-P-7A ACFT ENGINE |