fuel system configuration now. single fuselage tank, gravity feed with boost pump only. fuel path goes from fuselage tank to fuel valve, fuel valve to tee from tee one line goes to boost pump 2nd line goes thru check vavle then to gasalator then thru tee on discharge side of gasolator then to carb. From the boost pump line goes directy to tee on disharge side of gasolator then to carb. I would like to simplify system seems to be to many points of failure or leaks. Would this work fuselage tank to fuel valve to boost pump to gasolator to carb straight through system. This gives me the fewest conections. Any comments are appreciated.