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TF30-P-1 aircraft fuel control
material aluminum alloy, o/a dim. approx 2.102 in. min to 2.227 in. max lg by 1.972 in. min to 2.097 in. max w, rectangular eared flange w/4 holes, 2 top size 0.284 in. min to 0.286 in. max dia w/0.624 in. min to 0.675 in. max dia recess, segmented at top to 0.290 in. min to 0.330 in. max radius from center of hole, 2 bottom size 0.276 in. min to 0.286 in. max dia w/0.615 in. min to 0.635 in. max dia recess, 0.990 in. min to 0.010 in. max middle dia
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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.