What is the takeoff distance required for the Pilatus PC-12 NG at maximum weight?

The takeoff distance required for the Pilatus PC-12 NG at maximum weight is approximately 2,300 feet. This distance is determined through a series of performance calculations that account for various factors including aircraft weight, runway conditions, altitude, and temperature. The PC-12 NG is designed for versatility in various operational environments, and its performance metrics reflect its efficiency and capability, particularly in shorter runway scenarios.

When at maximum weight, the aircraft requires sufficient runway length to achieve the necessary speed for lift-off while also ensuring that safety margins are adhered to. Factors such as engine power, wing design, and aerodynamic efficiency play critical roles in determining the specific distance needed. The performance charts in the pilot's operating handbook (POH) provide the most accurate data, supporting the figure of approximately 2,300 feet for takeoff under maximum weight conditions.

Understanding these performance parameters is crucial for pilots, especially when planning flights that may involve takeoffs from airports with limited runway lengths. Proper knowledge in this area can greatly impact flight safety and efficiency.