Hi everyone! A quick question about the KR2's VNE. I know it is officially 200mph, is that IAS or TAS? I know some planes have exceeded this, what would be a safe figure for a KR2 without elevator or rudder counterbalances? I know this is not s simple question I am just looking at an approximate figure.
I am really more interested in high altitude (lets say 20K feet) speed where the difference between IAS and TAS becomes significant. Thanks! Fly safe, Rudi
