Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-033-9081 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: 4047224, 2840-01-033-9081, 01-033-9081, 2840010339081, 010339081
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 14, 1977 | 01-033-9081 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-033-9081
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4047224 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-033-9081
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM |
| DIAMETER | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM |
| SPECIAL FEATURES | INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; SEE TCTO 2J-F100(II)-509 SUPERSEDES PN 4036639; F100 FRACTURE CRITICAL PART. |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,PLAIN,ROUND |