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J57 aircraft engine
steel, aisi 302 or 303; 0.320 in. min, 0.330 in. max thk, 0.682 in. min, 0.685 in. max dia; groove 0.14 in. w, 0.508 in. min, 0.517 in. max dia; flange one side 0.03 in. thk, 0.738 in. min, 0.740 in. max dia; center hole 0.18-0.22 in. dp, 0.28-0.31 in. dia, tap .250-28NF-2, dp .12 min full thd; part of surge and temp limiting valve assy for main fuel control, jfc 8
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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 j57 aircraft engine.