Used on heavyweight torpedo engine assembly stand. 1.5000" overall length headless press fit type-p matt- 52100 tool steel, heat treated 62/64 rc, all press fit bushings are lapped, honed, or gound in the i.d. bushing with i.d. of 1/8" to 1" are concentric with 0.0003" t.i.r. to the o.d. all unground bushing are left rough on the o.d. with concentricity of appx. ".006" t.i.r> no-counterbore bushing are standard with acme. 17c solid, plain, no outside flanges
Used on special aircraft and engine tool/support equipment/parts. altered item drawing-make from T113/cage 60038 send bearing to cage 3XWW5 to have bearings treated with micropoly lubricant (temp range -50 to +225 f)
Used on 1055-01-450-4243 multiple launch rocket system (mlrs). angular bearing 0.25 inch thick, 0.25 inch wide, ; angular contact single bearing; standard circular pocket formed ring seperator; 0.125 inch balls, type a, precision class 1
Used on f/a-18e/f. 0.6350" overall length (navy) bushing, sleeve, aircraft chamfer 0.005 to 0.015 x 45deg; 1hole in middle; bushing-clamp-up; not intended for reaming on assy-designed for clamping to shaft with relative motion occurring on bushing od only@ passivate body surface treated 17c solid, plain, no outside flanges
Used on amad(airframe mounted accessory drive); f-18 aircraft. 0.6691" bore diameter inner roller bearing, matched pair this is a matched pair of bearings 262a single row, two lip inner ring, no outer ring, roller retainment rings, non-separable
