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National Stock Number: 2840-01-216-0526
Federal Supply Class: 2840
National Item Identification Number: 012160526
Description: HUB,COMPRESSOR,AIRCRAFT GAS TURB
Detail: 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.
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Manufacturer Information:
4067357 | 77445 | RTX CORPORATION |
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Techincal Specification:
MATERIAL | NICKEL ALLOY HUB | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB | 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; REIDENTIFIED FROM P/N 4047224 | CRITICALITY CODE JUSTIFICATION | APGF AND | | CZBJ AND | | CZCJ AND | | ABHP AND | | ABMZ | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,DRIVE SHAFT | THE MANUFACTURERS DATA | | MANUFACTURERS CODE | 77445 | DESIGN CONTROL REFERENCE | 4067357 |
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