Fokker 50 PEC fault
In the F50, when a Prop Electronic Control fails the Np will go to 104%
The QRH then states that a speed limit of 220 knots TAS (not IAS) applies.
Anyone know why this limit would be a TAS and not an IAS?
It's definately not a typo in the QRH as a table is provided for you to work out TAS limits at various levels based on IAS.