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F100-PW-200 aircraft engine
alum alloy per ams 4117; length 1.069 in. nom; HEX-Sided end 0.808 in. nom across flats, 0.070 in. dia hole thru each flat to 0.13 in. dp counterbore 0.562 in. dia, center hole drill 0.296 in. dia; other end 0.5625-18UNJF-3A thd; part of filter and plug assy 767103-2 for backup fuel control p/n 768000
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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 f100-pw-200 aircraft engine.