fuel flow test 914
A "typical" fuel flow test whereby one puts the aircraft in an extreme nose up attitude and then disconnects the hose at the carburetor, does not seem logical because the pumps will need to be turned on, and the fuel flow will likely be in the 35 gph range (the 914 requires only 8.7 gph at takeoff performance).
Doing a gravity test at the pump inlets also doesn't seem all that helpful because the pumps have considerable suction and can undoubtedly deliver far more fuel than gravity alone.
Suggestions?