Serving our customers with quality and safety first.
cres ams 5612 per hamilton std spec hs 178, hardness rockwell superfical R15N, 75.0-79.5, heat treat per hamilton std spec hs 461, 0.56 in. o/a lg, 0.6243 in.min 0.6245 in.max dia left end, 0.53 in.dia right end
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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.