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Old 06-28-2016 | 08:52 AM
  #15  
PT6driver
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Originally Posted by clipperskipper
What everyone failed to remember here, is the simple fact that there is a reduction gear box connected to this thing, hence the maximum continuous horsepower ratings. If you have ever seen one come apart, it's uncontained, and parts will wander through the fuselage.
I don't care to ever see one come apart.

Originally Posted by JohnBurke
Who told you that?

Torque is a limiting value, as is temperature.

In many cases, turbine installations have torque limits that aren't due to the engine, but for the airframe.

Torque is usually a limiting factors at lower altitudes and cooler days, and temp at higher altitudes and hotter days.

If you hit a torque limit or a temp limit first, you stop. Some days you're torque limited, others temp limited, depending on the conditions and location, for departure, and nearly always temp limited in cruise at higher altitudes.

Be careful about the rumors and wives tales that you'll her about Pratt said this or that...I recently talked to a pilot who was convinced that while he had a five minute allowance, he could simply back off to a lower temperature and then go back to the five minute overage again...and again...and again. His reasoning was that it was five minutes at a time, and that so long as he only did five minutes, he could keep doing it. Not so.
Ha. I'm just a bit sharper than that guy and understand the 5-minute limitation. I'd hate to see what he would run in a turbocharged piston with a time limitation. Trust me, I don't go run an engine based off of an OWT. That's a big pet peeve of mine.

As I've said, I was just looking to find the reasoning behind the operation. Platus's POH says one thing, we operate another way, and then Finoff Aviation's calculator has their own numbers. (seen here: Free Pilatus PC-12 Power Calculator from Finnoff Aviation). Just making sense of it all.

The unused range from our operating ITT to the Max. Continuous ITT is just mainly for longevity and ease of operation on the engine. It won't kick itself out of the airframe for running there for however long necessary assuming we're also under the TQ limitation.
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