Used on aircraft models sh-3a/d. components include plunger 1; cap 1; cover assy 1; cover sub assy 1; by-pass valve 1; spring 1; filter element 1; bowl assy 1
opr temp fuel: 65.0 to 135.0 degrees f; pressure fuel: 0 to 135 psig operating, 270 psig proof 7500 psig burst; 15.46 max. in. lg., 7.43 max. in. w.; 23 gpm hydraulic oil supplies at 2700 psid max. to hydraulic motor on fuel pump will deliver 220 gpm of jet