0.7037" overall width 3.5665" bore diameter 0.00008 in. max variation in dia of rollers 250a single row, non-locating, two lip inner ring, cylindrical outer ring with two roller retainment rings on outer, non-separable
0.6249" overall width 2.0680" bore diameter bearing stabilized for operation from m 65 to p 300 deg f, 0.00008 in. max variation in dia of rollers 252a single row, non-locating, two lip inner ring, cylindrical outer ring, separable
0.7037" overall width 1.2793" bore diameter this item is on the csi list for air force 252a single row, non-locating, two lip inner ring, cylindrical outer ring, separable
Used on f100 engine. 0.5462" overall width 1.3778" bore diameter inner 254b single row, one-direction locating, one lip inner ring, one lip outer ring with one roller retainment ring on outer, separable
Used on f15/f16 acft. 1.5000" overall width 100.0mm bore diameter pin 0.1241 in. nom dia required to complete assembly; cage to be silver plated 0.001-0.002 thk per ams 2412 onland riding surf 252a single row, non-locating, two lip inner ring, cylindrical outer ring, separable
0.4670" overall width 0.6693" bore diameter heat stabilized at m 65 deg f to p 300 deg f 252g single row, one-dirction locating, one lip inner ring, one lip outer ring, separable
0.8130" overall width 35.0mm bore diameter 250a single row, non-locating, two lip inner ring, cylindrical outer ring with two roller retainment rings on outer, non-separable
2.1250" overall width 60.00mm bore diameter 0.3750 in. blind hole in od 252b single row, non-locating, cylindrical inner ring, two lip outer ring, separable
25.0mm overall width 40.0mm bore diameter 250a single row, non-locating, two lip inner ring, cylindrical outer ring with two roller retainment rings on outer, non-separable
1.1875" overall width 40.0mm bore diameter 250a single row, non-locating, two lip inner ring, cylindrical outer ring with two roller retainment rings on outer, non-separable
