Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-458-2760 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: 784473, 2840-01-458-2760, 01-458-2760, 2840014582760, 014582760
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 19, 1998 | 01-458-2760 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-458-2760
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 784473 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-458-2760
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 12.726 INCHES NOMINAL |
| DIAMETER | 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM |
| SPECIAL FEATURES | P/N NEVER TO BE PROCURED; REWORKED AND REPAIRED; IF P/N 635498 HAS CRACKS IN THE TIE ROD HOLES IT WILL BE RE-ASSIGNED TO THIS P/N |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AFEAT$$AABMZ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 6, IND 51 |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT GAS TURBINE ENG |