Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-159-6846 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: 624359, 2840-01-159-6846, 01-159-6846, 2840011596846, 011596846
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 12, 1983 | 01-159-6846 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-159-6846
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 624359 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-159-6846
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 5.800 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG34 IND52 |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HUB ASSEMBLY OF,TURB ROTOR |