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main fuel control for J57-43W aircraft engine
chamber 3.96 in.l, 0.44 in i/d, second chamber 0.90 deg. 0.821 in.i/d, 2 holes 0.70 depth 24 UNC-2B thd located within 0.005 radius 1.38 dia
acft fuel system
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 main fuel control for j57-43w aircraft engine.