What is the stall speed in landing configuration for the Pilatus PC-12 NG?

The stall speed in landing configuration for the Pilatus PC-12 NG is 71 knots. This speed is critical for pilots to know, as it represents the minimum speed at which the aircraft can maintain controlled flight during the landing phase. Understanding stall speed is essential for safe landing operations, as flying below this speed can lead to a stall, risking loss of control.

In the landing configuration, which typically includes flaps extended and gear down, the aircraft’s stall characteristics change due to increased lift produced by the wing’s camber. Recognizing the stall speed helps pilots establish an appropriate approach speed, ensuring they maintain a safe margin above this critical value during landing. In practice, pilots will typically aim to approach the runway at a speed well above 71 knots to provide an added safety buffer and maintain control of the aircraft.