Serving our customers with quality and safety first.
J57 and T33 aircraft engine fuel manifold
material felt, o/a dim. approx 10.200 in. lg by 0.200 in. min to 0.300 in. max thk, irregular shaped, middle 2.310 in. w w/2 flaps, top flap 0.980 in. lg, bottom flap 2.550 in. lg w/45 deg tip angle to 2.340 in. lg, right end 1.640 in. w w/2 flaps on end 0.400 and 0.260 in. w, left end 1.100 in. w w/2 flaps 0.440 and 0.400 in. w
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 j57 and t33 aircraft engine fuel manifold.