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F100 acft engine fuel fan exit temp sensor, model TS-U1
0.656 in. o/a lg, OVAL-Plano shape flange 0.930 in. lg by 0.460 in. w by 0.060 in. thk w/2 holes 0.140 in. max dia spaced 0.680 in. c to c and 0.250 in. middle inside dia, groove 0.080 in. max w around side, 0.190 in. dia small end w/0.120 in. inside dia
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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 acft engine fuel fan exit temp sensor,model ts-u1.