What is the purpose of the Maximum Operating Range (MOR) in the Pilatus PC-12 NG?

The Maximum Operating Range (MOR) in the Pilatus PC-12 NG serves a crucial role in managing engine power during an in-flight system failure, particularly when delivering optimal performance in emergency situations. When a malfunction occurs, the MOR allows the pilot to operate the engine at maximum power settings safely and efficiently, ensuring the aircraft can maintain control and perform necessary maneuvers.

In aviation, managing engine power is vital for aircraft safety, especially during critical phases of flight. The MOR assists in determining the limitations of engine output to prevent damage and maintain operational integrity. This is particularly important when pilot decision-making is involved for extraordinary circumstances such as an engine failure.

Understanding this function highlights the importance of the MOR in enhancing flight safety and operational effectiveness. The other aspects mentioned, like fueling the aircraft during ground operations or adjusting landing gear deployment, are not connected to the MOR's purpose, while cabin pressure regulation has a separate dedicated system entirely. Thus, the primary focus of the MOR is firmly on controlling engine power to ensure a reliable response during system failures.