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F100 acft engine fuel fan exit temp sensor, model TS-U1
0.545 in. o/a lg, oval shape flange w/ears, 2 holes 0.140 in. max dia spaced 0.680 in. c toc, hole in. ear 0.040 in. dia, inside opening 0.250 in. dia
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 f100 acft engine fuel fan exit temp sensor,model ts-u1.