Serving our customers with quality and safety first.
lever, connecting, 83 min, 87 max rockwell 15n scale hardness, 0.124 in. o/a w, 0.095 in. offset height, 1.000 in. c to c distance between link and shaft holes, 0.375 in. shaft end thk, 0.225 in. min, 0.235 in. max link end thk, 0.0935 in. min, 0.0943 in. max link end 1st hole dia, 0.0940 in. min, 0.0948 in. max link end 2nd hole dia, 0.094 in. distance from 1st link hole center to end, 0.500 in. c to c distance between 1st and 2nd link hole centers, 0.0940 in. min, 0.0948 in. max clamp hole dia on one fork tongue, 0.0923 in. min, 0.0931 in. max clamp hole on opposite fork tongue, 0.113 in. min, 0.117 in. max distance between fork inside spread, connecting link, rigid, cres AMS5525, 24 min, 37 max rockwell c scale hardness, 2.375 in. o/a lg, 2.123 in. min, 2.127 in. max effective lg, one hole each end, 0.0935 in. min, 0.0943 in. max dia, 0.125 in. end radius each end, 0.100 in. body w, 0.107 in. min, 0.111 in. max body thk, pin, straight headless, cres, HS2776, 0.360 in. min, 0.370 in. max lg, 0.0932 in. min, 0.0934 in
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.