aluminum, 2.812 in. w, 2.906 in. h, 0.187 in. thk, three 0.203 in. dia mtg holes on the corners of an isosceles triangle, base 2.000 in., altitude 2.188 in.
steel, carbon, hr or cr temper no. 3, 4 or 5 spec qq-s-698, 0.1196 in. thk sheet or 0.120 in. thk strip cadmium plated, type 2, class 3, spec qq-p-416, 2.250 in. o/a lg, 1.490 in. o/a w, c/o one bracket fscm 19207 part no. 11678154-1, one guard fscm 19207 part no. 11678154-2, one mounting hole, 0.660 in. min id, 0.720 in. max id
stainless steel, 1.13 in. min, 1.15 in.max lg, 0.543 in. min, 0.557 in. max w, 0.318 in. min, 0.327 in. max h, 0.012 in. min, 0.018 in. max material thk
aluminum, iridescent yellow finish, accommodates 2 push button switches, 1.160 in. lg, 1.430 in. w, 2.780 in. h, 4 no. 4 /0.112 in./ -40 thd mtg holes on 0.800 in. by 1.160 in. mtg centers
Used on landing vehicle. cres, qq-s-766 type 302 or 304, passivated, 1.500 in.lg, 1.380 in.w, 1.000 in.h, center hole 0.475 in.min, 0.500 in.max dia, 4 0.187in.min, 0.203 in.max dia mtg holes on 0.875 in.mtg centers
bracket matl only black oxide, per mil-c-3924 class 1, prior to assembly; 1.539 in. lg; 1.365 in. w; 0.421 in. h; 1.179 in. of lg has 1.830 in. curved radius with 0.360 in. flat extension; surface roughness 125 per usab.1-62; 2 self-clinching nuts 0.136 in. dia thru matl; clip component/tubular rivet 0.093 in. plus 0.003 in. or minus 0.001 in. dia thru matl; consists of bracket, component clip, tubular rivet, self clinching nut/epoxy cement (shell)
Used on aircraft model f-8. beryllium copper 1/2 hard per qq-c-533, 0.020 in. thick; 2.875 in. lg; 0.625 in. w; 0.531 in. h; cadmium plate per qq-p-416, type 2, class 2
