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29159778578
cres AMS5610 or cres per united aircraft corp. spec no.H178, rockwell hardness rating rc 30-38, 0.360 in. o/a lg, 0.970 in. min, 0.980 in. max flange od, 0.060 in. flange width, countersink 90 deg, 0.250 in. min, 0.280 in. max body id, 1/4-28 UNF-2B thread data, 30 deg, 0.130 in. lg of chamfer, 0.483 in.min, 0.493 in. max body od on second end
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.
Used on 29159778578.