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cft, 68A552002-1003, F15 acft
ialum alloy 6061-T651 per QQ-A-225/8; 12.310 in. min, 12.430 in. max lg o/a; induce inlet mtg plate holes 3 places 1.440 in. from center inlet hole; mixing tube flange 2.0 in. sq.max, 1.25 in. end od; motive port per MS33649-8, 2.31 in. CEN-TO-Inlet place face, 1.90 in. TOP-TO-Cen motive nozzle; fuel per MIL-T-5624, motive flow 2.5 gpm max, induced flow (steady state alt) 8.5 gpm min at alt s.l. to 30kft, then varying linearly w/alt to 4.0 gpm min. at 45kft alt.
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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 cft,68a552002-1003,f15 acft.