Serving our customers with quality and safety first.
cres AMS5613 or QQ-S-763 class 410, rockwell c scale 30.0 min, 38.0 max hardness, 1.855 in. min, 1.865 in. max o/a lg, link end 1st hole, 0.0947 in. min, 0.0957 in. max dia, 0.125 in. end radius, link end 0.030 in. min, 0.040 in. max lg, 0.210 in. w, 0.250 in. radius offset located 0.480 in. min, 0.520 in. max from link end on one side, 0.510 in. min, 0.550 in. max offset 0.250 in. radius opposite side, shaft end, 0.245 in. min, 0.255 in. max fork width, 0.0945 in. min, 0.0965 in. max fork span width, 0.350 in. min, 0.360 in. max fork depth, 0.1380 in. from link end hole center to shaft end fork
1EA
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.