Used on f-16 acft. 0.0880" first hole diameter 0.5800" overall length groove dia 0.0900 porm 0.0200 in.center 0.4400 in. from flange face passivate surface treated 22c solid, external flange one end
Used on f-16 acft. 0.0880" first hole diameter 0.7700" overall length holes located on grooves 0.4400 in. from flange face cadmium surface treated 22c solid, external flange one end
Used on f-16 acft. 0.5000" overall length item is not csi but has critical features such as tolerance, heat treatment, surface finish, or fluorescent penetrant inspection passivate surface treated 17c solid, plain, no outside flanges
Used on f-16 acft. 0.0880" first hole diameter 1.7600" overall length holes on 2 grooves centers 1.190 in. from flange face; inner groove width 0.090 porm 0.020 in. depth min 0.1395 max 0.1502 in.; outer groove width 0.120 porm 0.020 in. depth min 0.0415 max 0.0522 in. 22c solid, external flange one end
Used on f-16 acft. 0.0880" first hole diameter 0.8500" overall length holes on 2 grooves, centers 0.4700in. from flange face; inner groove width 0.090 porm 0.020 in, depth 0.073porm 0.005 in.; outer groove width 0.120 porm 0.020 in. depth 0.175 porm 0.005 in. 22c solid, external flange one end
Used on aircraft f-16,general dynamics. 1.0600" overall length right end counterbored 0.380 in. deep with 1.120 in. dia. 22c solid, external flange one end
Used on f-16 acft. 0.1870" first hole diameter 0.5680" overall length both flanged ends are cutaway 0.005/0.010 in. wide anodize surface treated 18c solid, external flanges both ends