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F101-GE-102 eng, B1-B acft
main fuel connection airframe to engine
14.063 in. from flange face to coupling end, 8.14 in. C-TO-C INLET-TO-Outlet; flanged end has 6 holes thru 0.280 - 0.285 in. dia on 4.50 in. bcd, part of gimbal assy 10630-69-109; center gimbal assy p/n 10630-69-105; coupling end 3.392 in. max od, part of pin joint assy 10371-40-1; opr press. 4psig neg to 120psig pos; media JP4 & JP5; temp range internal -65 to 285 deg f, external -65 to 400 deg f; aprox wt 7.70 lbs
1EA
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 f101-ge-102 eng,b1-b acft.