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ab fuel control 7086M35 for F101-GE-102 aircraft engine
halum alloy per AMS4117; mtg flange 0.23 in. thk w/hole thru each end 0.212 - 0.218 in. dia 1.576 in. apart C-TO-C; center stem 0.85 in. h, 0.49 in. od, tap drill 0.222 in. dia thru 100 deg csk 0.33 in. dia, 0.3125-24UNJF-3B, 0.63 in. min dp; base 0.609 in. dp, 0.845 - 0.850 in. id, seal groove 0.090 - 0.100 in. below flange, 0.135 - 0.140 in. w, 0.97 in. nom dia, 4 holes eq sp 0.124 - 0.129 in. dia 0.16 in. from CEN-TO-Bottom; part of sensor assy, p/n 7033M64G06
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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 ab fuel control 7086m35 for f101-ge-102 aircraft engine.