Serving our customers with quality and safety first.
cres, ams 5513 or ams 5515 per united aircraft spec hs 178, 1.170 in. min, 1.210 in. max o/a lg, 0.500 in. min, 0.540 in. max o/a w, 0.750 in. center to center distance between holes along length, 0.186 in. min, 0.192 in. max 2 bolt hole dia, chamfer 45 deg porm 5 deg by 0.125 4 places
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.