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A7 aircraft fuel control, p/n 2-155-152
material aluminum alloy, anodized finish, circular w/eared flange, o/a dim. approx 4.992 in. dia w/inside dia of 4.520 in., by 2.241 in. min to 2.259 in. max w, 6 holes, 0.201 in. dia, equally spaced on 4.656 in. bcd, SQ-Eared flange, 3.000 in., on front w/4 holes, 0.323 in. dia, spaced 2.370 in. min to 2.380 in. max c to c, center opening 1.780 in. min to 1.785 in. max dia
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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.
Used on a7 aircraft fuel control,p/n 2-155-152.