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J57 aircraft engine
cres per ams 56108 immunize, heat treat RC35-45; 1.406 in. l, 0.37175 in. dia; head 0.3125-24UNF-2A thd, hex socket 0.1562-0.1582 in. across flat, 0.218 in. dp, hole thru 2 walls 0.070 in. dia; stem 0.250-28Ns thd 0.342 in. from end, point 0.188 in. dia; part of cam body group for main fuel control model AJ-A2
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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.