What is the maximum continuous engine ITT during MCT?

The maximum continuous engine Inter-turbine Temperature (ITT) during Maximum Continuous Thrust (MCT) for the Dassault Falcon 7X is specified as 920°C. This temperature limit is established to ensure that the engines operate safely and efficiently while providing the required thrust. Exceeding this temperature can lead to excessive wear and potential damage to the engine components, ultimately affecting the aircraft's performance and reliability.

MCT is a power setting that pilots use during flight, especially in scenarios where maximum thrust is needed over extended periods, such as during climb-outs and while flying in adverse conditions. The ITT is a critical parameter in monitoring engine health, and adhering to the specified limits helps maintain optimal performance and longevity of the engines.

When considering other temperature limits associated with MCT, while there are specified thresholds for different operational phases, 920°C is the maximum continuous ITT tolerated for MCT, ensuring that pilots can operate the Falcon 7X with confidence in the engine's operational integrity.