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TF30-P-1 aircraft engine fuel system, p/n 464200
ams 5613 stainless steel w/ROCKWELL-C 35 to 40 hardness and chromium plate, o/a dim. 3.580 in. min to 3.600 in. max dia by 1.460 in. deep, right end 3.320 in. min to 3.340 in. max dia w/3.217 in. min to 3.219 in. max inside dia, left end 3.049 in. min to 3.053 in. max dia w/2.905 in. min to 2.925 in. max inside 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 engine fuel system,p/n 464200.