as i recall(i'll have to look it up again) but vne is 274 kts in a ivp.
if this is the case then it must be indicated not true otherwise i as
would most iv and propjet drivers exceed vne in cruise at 300+ ktas at
altitude with indicated around 200.  am i missing something?

david weinsweig
n750dw propjet(still for sale)
304-633-5221
weinsweigd@gmail.com