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F15 and TF15 acft engine fuel system, p/n 2710941M1
aluminum alloy w/anodized finish, withstands 120 psi air pressure, o/a dim. 1.5515 in. min to 1.5609 in. max dia by 1.738 in. min to 1.752 in. max lg, EARED-Flange w/4 holes 0.156 in. min to 0.161 in. max dia equally spaced on 1.800 in. bcd and 0.982 in. max inside dia left end, 6 notches 0.030 in. deep and 1.317 in. max inside 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.
Used on f15 and tf15 acft engine fuel system,p/n 2710941m1.