The total aircraft weight is used to determine the pull test required. To have the proper safety factor the pull test weight is determined by the total flying weight of the airplane. Since the pull test is now based on a multiple of the airplane weight there is no advantage or disadvantage for the type of propulsion system when it comes to the pull test. The same airplane with electric power will normally weigh more than that airplane with fuel power. Therefore it is reasonable and proper for the heavier airplane to have a higher pull test. There is no advantage to the fuel powered airplane in the pull test. A 30 oz. Ringmaster has a lower pull test than a 48 oz. Ringmaster whether they are both electric or IC.
There is no handicap given to fuel powered airplanes for governors or timers on electric airplanes.
Pat
Your logic is flawed!
Electrics take off with the full safety factor and maintain that for the entire flight.
Gas planes take off with a reduced safety factor because they are weighed without the fuel. Thus their safety factor is less at the beginning (because they weigh more then) and at landing they finally match the electrics.
Therefore, there is an advantage to the gas powered planes. The point of where they have to switch line sizes for the same safety factor is lower, thus some are able to fly on thinner lines that the "equivalent" electric.
Might me time to consider weighing with a full fuel load!