Description:

0.6250 inches bore diameter, 1.9375 inches overall outside diameter, grease lubrication material, 0.5000 inches outer ring width.

Special Features:

880 percent of mil-g-81322, internal radial clearance 0.0004 in.Min, 0.0010 in. Max heat treat rings and balls to rockwell c 60 to 66 and stabilized for operation at 250 degrees f, radial and lateral eccentricity inner ring 0.0010 in. Outer ring 0.0016 in.

Properties:

A cylindrical item in which the inner or outer ring turns upon row(s) of hardened ball, bearing which roll on a raceway, thus minimizing friction. These items are characterized by their noncorrosive qualities, lightness of weight, inch dimensions rather than metric, inner rings generally projecting beyond the faces of the outer ring, or a very narrow width inner ring having an outside diameter slightly larger than the bore diameter. Designed primarily for use in aircraft assemblies, such as control systems and surfaces of aircraft. Excludes bearing, ball, annular.