Recently I found out, that at higher speed (over 100kt) I get approx. 10kt difference between IAS and CAS (IAS and TAS is to high), at 70kt it is fine. The source of error is likely pitot location, which cannot be changed. Based on wrong TAS I get also wrong wind calculation.
I cannot find any possibility in Skyview to define airspeed corrections. I think, making software feature for CAS calculation would not be complicated.
I cannot find any possibility in Skyview to define airspeed corrections. I think, making software feature for CAS calculation would not be complicated.