Now that I have the wheel fairings and pants installed I did a few runs today to get some performance numbers for planning etc. I wondered how they compare to others with similar setup. Plane is not yet painted. Numbers are from the Dynon D100.
Altitude RPM MAP %Power TAS (MPH) Fuel Flow (gph)
8500 2300 17 50 160 6.5
8500 2400 19 60 170 7.9
8500 2700 22 77 192 10.5
Leaning was a either peak or 50 deg ROP using the Lycoming technique and watching the Dynon. OAT was 41F. At the WOT setting the RPM would exceed 2700 which surprised me, I have the Van's recommended sensenich prop which I believe is 85 inch pitch. Aircraft weight was about 1550 lbs.
Altitude RPM MAP %Power TAS (MPH) Fuel Flow (gph)
8500 2300 17 50 160 6.5
8500 2400 19 60 170 7.9
8500 2700 22 77 192 10.5
Leaning was a either peak or 50 deg ROP using the Lycoming technique and watching the Dynon. OAT was 41F. At the WOT setting the RPM would exceed 2700 which surprised me, I have the Van's recommended sensenich prop which I believe is 85 inch pitch. Aircraft weight was about 1550 lbs.