We have completed our fuel system testing! Our understanding is that while its not technically required, we felt more comfortable verifying prior to first takeoff that we had ample fuel flow to our O540.
So we installed the wings temporarily:

And rigged up a fuel can and timer to document fuel flow, we were using a postal scale to weigh the amount of fuel and converting to come up with a volume amount.

We then set the fuselage at an 18 degree climb angle, with 4 gallons of fuel in either main tank. This was what we considered a bare minimum fuel level in the tanks, at this attitude we "just" began to see fuel level in our fuel level gauges.
After our first test, we found we were getting much less than we had initially anticipated. Using the FAA approved calculation based on BHP of the engine, we required 32 gallons/hr fuel flow for our Lycoming O540 fuel system and were getting much less than that with the electric pump. Something didn't seem right with the electric pump, and we started to suspect that it was faulty after checking over the rest of the fuel system. After scratching our head for a while, we determined that the pump we had been sent was a 24V pump instead of the required 12V version (they look the same). We then isolated the pump electrically and rigged up a 24V DC power supply, and tested again.
Our second test with the pump properly supplied with DC and 3.5 gallons in either tank (fuel selector on "both") was 36 Gallons an hour!

Muy Bueno!
So that made us feel confident that we had more than enough fuel supply in any situation we could foresee. We took the wings off, ordered the correct 12v pump, and installed it. We are headed to the airport this next week!
