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TF30-P-1 aircraft fuel control
material stainless steel, rockwell c 35 to 40 hardness, 0.620 in. dia each end, approx 0.370 in. lg by 0.189 in. min to 0.190 in. max w middle section, 2 holes, 0.405 in. min to 0.425 in. max dia, one on each end and spaced 0.950 in. c to c
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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 tf30-p-1 aircraft fuel control.