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Turbine Inlet Temperature (TIT)
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Category: | Flight Technical | ![]() |
Content source: | SKYbrary | ![]() |
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TIT (Turbine Inlet Temperature)
Description
Turbine Inlet Temperature (TIT) is the temperature of the combustion chamber exhaust gases as they enter the turbine unit. The gas temperature is measured by a number of thermocouples mounted in the exhaust stream and is presented on a flight deck gauge in either degrees Fahrenheit or degrees Celcius.