Hello,
I’m still in the testing phase at the moment, but I’m considering purchasing VFRNAV.
To eliminate paper planning, I’m still missing two vital points:
(I fly in a mountainous region with an aircraft type that has a center tank in front of the pilot)
1)The weight-and-balance calculation must display the tank fuel level as a straight line in the graph. With baggage the aircraft could become tail-heavy when the tank is flown empty.
2)The takeoff and landing distance depends on density altitude. A calculation of this including further factors is important. Tabular, with custom safety margins