How does the Pilatus PC-12 NG handle asymmetric thrust in-flight?

The Pilatus PC-12 NG is a single-engine aircraft, meaning it relies on one engine for thrust. In the event of thrust asymmetry, which can occur if the aircraft experiences a significant change in engine power or a malfunction, the pilot must actively manage the aircraft's stabilization. The correct approach involves the application of appropriate control inputs to counteract the yaw that results from the asymmetric thrust.

Asymmetric thrust creates a yawing motion about the aircraft's vertical axis, pushing the nose to the side of the reduced thrust. To maintain control and safety, the pilot needs to use the ailerons and rudder to counteract this effect and keep the aircraft flying straight. The rudder is particularly important, as it generates the required side force to counter the yawing motion created by the imbalance.

The other methods listed, such as deploying flaps, adjusting the throttle on the opposite engine, or using differential braking, do not effectively address the issue in the context of the PC-12 NG, as it doesn’t have multiple engines or the specific configurations that would necessitate those actions for managing asymmetric thrust. Thus, the necessity for pilots to apply the correct control inputs to counteract yaw is crucial for maintaining flight control in such situations.