Anyone tried testing the fuel lines before the forward skin/panel is put on while everything was open? I thought about putting tubing on the fuel line where it exits the fuselage and into a can of gas. Then activating the electric fuel pump and having the gas exit through the gascolating again with fittings and tubing attached. Precautions taken because of working with the volitility of the fuel. Maybe this isn't necessary, but it would save efforts if there was a fitting leak.