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TF30-P-1 aircraft fuel control
material stainless steel, ROCKWELL-C 45 to 50 hardness, o/a dim. 0.996 in. min to 0.998 in. max dia by 1.989 in. min to 2.011 in. max lg, 0.655 in. min to 0.657 in. max inside dia, large end dim. 0.800 in. min to 0.820 in. max dia w/fitting 0.862 in. min to 0.862 in. max dia, 10 holes 0.089 in. min to 0.099 in. max dia equally spaced on side, small end dim. 0.605 in. min to 0.615 in. max dia w/fitting 0.887 in. min to 0.891 in. max dia, 0.580 in. inside dia, 6 holes 0.111 in. min to 0.121 in. max dia equally spaced on side, groove 0.095 in. min to 0.105 in. max w around side
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.