I have a question on sulfidation.
As I recall in flying the Cheyenne and Commander (although it's been a few months since I've been in any turbine) at low altitudes you're several hundred degrees below maximum continuous, and really can't get close without overtorquing. I may be recalling incorrectly, but it's not an altitude I need to fly at since we just go to FL200+ and have no problems getting the temps nice and warm. So this is the nature of my question.
Let's take something like a Caravan or Beech 99, or any of the turbine crop dusters. They're relatively unlikely to fly above 10,000 ft on a regular basis. The Caravans out of here fly at 5,000-6,000 ft for most of their lives. Do these aircraft have more sulfidation issues? Or are they actually able to get the temps high enough that it's not an issue? Is there something different about these engines to optimize for low altitude?