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J57 and T33 aircraft engine fuel manifold
amaterial felt, o/a dim. approx 10.800 in. lg by 0.200 in. min to 0.300 in. max thk, middle 1.300 in. lg by 2.400 in. w, identical ends 1.100 in. w w/2 flaps on each end 1.060 in. lg by 0.380 in. w
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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 j57 and t33 aircraft engine fuel manifold.