The fuel system will be a standard wing tank system routed through a selector valve in the cockpit with engine driven and electric auxiliary fuel pumps.
One tank will incorporate a flop tube to sustain short periods of inverted flight.
The fuel system will be a standard wing tank system routed through a selector valve in the cockpit with engine driven and electric auxiliary fuel pumps.
One tank will incorporate a flop tube to sustain short periods of inverted flight.