6650-01-216-0525 ELECTRODE,SPECTROMETER Index 4920-01-216-0527 TEST STATION,FUEL CONTROL SYSTEM

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.


Manufacturer Information:
406735777445RTX CORPORATION


Techincal Specification:
MATERIALNICKEL ALLOY HUB
MATERIAL DOCUMENT AND CLASSIFICATIONPWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB
DESIGN TYPECOMPRESSOR
ENGINE SECTION LOCATIONCOMPRESSOR
STAGE NUMBER2
OVERALL LENGTH4.004 INCHES MINIMUM AND
4.014 INCHES MAXIMUM
DIAMETER7.162 INCHES MINIMUM AND
7.166 INCHES MAXIMUM
SPECIAL FEATURESINTL 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 JUSTIFICATIONAPGF AND
CZBJ AND
CZCJ AND
ABHP AND
ABMZ
PART NAME ASSIGNED BY CONTROLLING AGENCYORIG NAME NUT,DRIVE SHAFT
THE MANUFACTURERS DATA
MANUFACTURERS CODE77445
DESIGN CONTROL REFERENCE4067357


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