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TF30-P-1 aircraft fuel control
material stainless steel, ROCKWELL-C 35 to 40 hardness, o/a dim. approx 2.203 in. min to 2.258 in. max lg by 0.970 in. min to 0.986 in. max w, 2 holes, 0.093 in. min to 0.095 in. max on either side of middle section, large end dim. 0.490 in. min to 0.510 in. max dia w/6 slots, approx 0.190 in. min to 0.210 in. max lg by 0.073 in. min to 0.088 in. max w, equally spaced, fitting approx 0.047 in. min to 0.078 in. max radius by 0.080 in. min to 0.100 in. max thk, small end dim. 0.270 in. min to 0.290 in. max w w/slot approx 0.360 in. min to 0.400 in. max lg by 0.103 in. min to 0.104 in. max w
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.