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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 0.0003 to 0.0005 in. thk, o/a dim. approx 4.5525 in. dia by 2.340 in. min to 2.380 in. max lg, concentric eared flange w/6 holes 0.339 in. min to 0.349 in. max dia equally spaced on 4.240 in. bcd, 3 thd inserts size 0.190-32 UNF-2B mod on flange front
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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.