What is the maximum continuous power output of the engine in the Pilatus PC-12 NG?

The Pilatus PC-12 NG is powered by a Pratt & Whitney Canada PT6A-67P engine, which is known for its reliability and efficiency in the turboprop segment. The engine has a maximum continuous power output rated at 750 shaft horsepower (shp). This level of performance strikes a balance between power, efficiency, and operational capability, allowing the aircraft to operate effectively in various flight conditions.

The designation of 750 shp is significant for pilots and operators as it defines the operational limitations and performance characteristics of the aircraft. Understanding the engine's power output is essential for planning missions, understanding climb performance, and managing fuel consumption during flight. The Pilatus PC-12 NG is designed to effectively utilize this power to achieve its impressive range and speed, confirming its status as a versatile and capable aircraft in the turboprop market.