Serving our customers with quality and safety first.
arm, cres, AMS5350, chrome plate, AMS2406, 26 min, 34 max rockwell chardness, 1.8745 in. min, 1.8755 in. max effective lg, 0.1250 in. min, 0.1255 in. max hole through each end on both sides, one end 0.940 in. w, 0.626 in. min, 0.632 in. max fork spread, opposite end, 0.630 in. w, 0.377 in. min, 0.383 in. max fork spread, roller, rocker arm, cam follower, cres, AMS5616, immunized, 0.3748 in. min, 0.3750 in. max od, 0.1252 in. min, 0.1257 in. max id, 0.154 in. min, 0.158 in. max w, shaft, straight, cres, AMS5616, 42 min, 50 max rockwell c hardness, immunized, 0.660 in. lg, 0.1246 in. min, 0.1249 in. max dia, one hole 0.040 in. min, 0.050 in. maxlocated 0.090 in. from one end, spacer, sleeve, cress, AMS5640, immunized, 75 min, 100 max rockwell b hardness, 0.185 in. min, 0.195 in. max od, 0.125 in. min, 0.127 in. max id, 0.053 in. min, 0.059 in. max thk
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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.