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TF30-P-1 aircraft engine fuel control, p/n 517600
ams 5355 stainless steel, chrome plate and ROCKWELL-C 35 to 42 hardness, o/a dim. approx 3.515 in. min to 3.535 in. max lg by 3.203 in. min to 3.246 in. max h by 2.287 in. min to 2.347 in. max wide, 1.150 in. min to 1.160 in. max dia right or lower end, triangular flange left or upper end w/3 holes 0.270 in. min to 0.286 in. max dia spaced 1.619 and 1.639 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 engine fuel control,p/n 517600.