NATO Stock Number
2805-00-737-3513
Sold in multiples of
1 EA
DEMIL
NO
Chamfer Angle In Deg
77.5 second end
Shoulder Length
0.062 inches second end
Chamfer Length
0.281 inches second end
Overall Length
12.688 inches
Undercut Diameter
0.365 inches first end
Undercut Diameter
0.370 inches second end
Undercut Width
0.109 inches first end
Undercut Width
0.125 inches second end
Body Outside Diameter
0.375 inches
Body Type
Tubular
End Length
0.3085 inches first end and 0.3165 inches first end
End Length
0.344 inches second end
End Length
0.3085 inches and 0.3165 inches first end
End Largest Diameter
0.382 inches first end and 0.386 inches first end
End Largest Diameter
0.500 inches second end
End Largest Diameter
0.382 inches and 0.386 inches first end
End Hardness Rating
Between 57.0 rockwell c and 63.0 rockwell c
End Casehardening Indicator
Casehardened
Flat Diameter
0.125 inches first end
End Spherical Radius
0.1865 inches second end and 0.1885 inches second end
End Spherical Radius
0.191 inches first end and 0.193 inches first end
End Spherical Radius
0.1865 inches and 0.1885 inches second end
End Spherical Radius
0.191 inches and 0.193 inches first end
Spherical Radius Depth
0.209 inches second end
Material
Steel
Material
Steel
Style Designator
Cup w/shoulder and chamfer second end
Style Designator
Spherical, undercut optional flat first end
Fsc Application Data
Gasoline engine, nonaircraft
