8120-01-668-9927 CYLINDER,COMPRESSED GAS,NITROGEN 3120-01-668-6925 BUSHING,SLEEVE

National Stock Number:
3040-01-669-2287

Federal Supply Class:
3040

National Item Identification Number:
016692287

Description:
SHAFT,SHOULDERED


Manufacturer Information:
803AS701-2230003NAVAL AIR SYSTEMS COMMAND MANAGED ORIGINAL DESIGN ACTIVITY NOT MATERIAL/PARTS SUPPLIER


Techincal Specification:
END SIMILARITYNOT IDENTICAL
FIRST END GROOVE WIDTH0.625 INCHES NOMINAL
FIRST END DIAMETER0.6240 INCHES MINIMUM AND 0.6245 INCHES MAXIMUM
FIRST END SPLINE LENGTH0.3125 INCHES NOMINAL
FIRST END SPLINE MINOR DIAMETER0.580 INCHES MINIMUM AND 0.582 INCHES MAXIMUM
FIRST END SPLINE QUANTITY36
FIRST END PITCH DIAMETER0.6050 INCHES NOMINAL
LARGEST STEP DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
MATERIALSTEEL CORROSION RESISTING
OVERALL LENGTH5.4375 INCHES NOMINAL
SECOND END HOLE DIAMETER0.1900 INCHES NOMINAL
SECOND END DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
SECOND END DISTANCE FROM HOLE CENTER TO END0.156 INCHES NOMINAL
SECOND END SLOT DEPTH0.625 INCHES NOMINAL
STEP QUANTITY2
SPECIAL FEATURESTHE SECOND END HAS A SLOT THAT GOES VERTICALLY THUR THE END OF THE SHAFT AND IS .251 +.001 -.000 IN DIAMETER, THERE IS A SIZE 10-32 UNF 3B HOLE THAT IS .156 INCHES FROM THE END INTO THIS SLOT, THIS HOLE IS 90 DEGREE COUNTERSUNK TO .215 DIA; THE SECOND HOLE ON THE SECOND END IS A NUMBER 4 TAPER HOLE; THE SECOND END IS 4.5 INCHES LONG; THE GROOVE IS BETWEEN THE FIRST AND SECOND END AND IS 1/16 INCHES WIDE; BOTH ENDS ARE CHAMFER 1/32 X 45 DEGREES


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