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aircraft engine fuel system, p/n 597700-1
operational flow 33 to 41 pph at 80 to 90 deg f w/98 to 102 psig pressure drop, optional flow direction, o/a dim. 0.348 in. min to 0.367 in. max lg by 0.360 in. min to 0.370 in. max dia, internal thd size 0.112-40 UNC-2B, small end 0.051 in. min to 0.061 in. max 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 aircraft engine fuel system,p/n 597700-1.