0.0994" overall width 0.0932" bore diameter 0.0003 in. inner ring radial runout 0.0006 in. outer ring radial runout, inner ring composed of two or more parts, stainless rivet type 303 soft, grace non-loading groove, non-separable
0.1875" bore diameter 0.0003 in. inner ring radial runout, 0.0006 in. outer ring radial runout removable shields, 0.5350 in. dia by 0.0550 in. w groove in. od of outer ring posistioned at 0.0860 in. from flange back face to be flat within 0.0005 in.
18.0000" overall width 55.0mm bore diameter internal clearance measured under 11 lb load, in accordance with lycoming turbine engineering spec E1004, heat stablized at minus 65 to plus 700 deg f, 3 oil holes 0.0310 in. dia spaced at 120 deg intervals 252a single row, non-locating, two lip inner ring, cylindrical outer ring, separable
26.0mm overall width 55.0mm bore diameter stabilized for operation at 65 deg f to p 350 deg f, thrust marking on od of outer rings, max surface finish, ball 2 uin aa, inner 92d counterbored outer rings, non-separable, tandem mounting
46.00mm overall width 65.00mm bore diameter in accordance with the premium aircraft quality rqmt of lycoming turbine engineering spec e 100, retainer silver-plated 0.0005 to 0.0015 in. thk per ams 2412, stabilized for operation at minus 65 deg to plus 600 deg, three grooves 0.0400 to 0.0500 in. wide by 0.0150 in. to 0.0200 in. deep equally spaced on inner faces of outer rings, thrust markings v etched on od 92d counterbored outer rings, non-separable, tandem mounting
0.3543" overall width 0.9843" bore diameter ufaces of inner ring sq w/bore within 0.0004 in., faces of outer ring sqw/od within 0.0004 in., parallelism ofouter non-loading groove, non-separable
7.0mm overall width 17.0mm bore diameter heat stabilized for operation at m 65 to p 350 deg f rockwell harness rating, retainer 47.0 min, rollers, inner 252f single row, one-direction locating, one lip inner ring, two lip outer ring, separable
