R
Ron Belliveau(Guest)
Guest
Transport Canada request a fuel flow test. They require you to prop up the aircraft in a 15 degree angle ( to simulate climb out) and require a 150% flow rate of the engine max burn rate. Our 360 engines require (with the 150%) 28 gph . A fuel flow test showed only 18.75 gph. After much checking and testing we found that by removing the floscan meter (last item in the line to carb.) we had a 33.75 gph flow. One would be lead to believe that there was a problem with the Floscan but we have two aircraft with each a floscan and the same results. 18.75 gph will not keep the 360 running at full power . What are we to do next?