Which of the following is a characteristic of normal law pitch control in the flight mode?

Normal law pitch control is designed to enhance the safety and handling characteristics of the aircraft. A fundamental aspect of this mode is that it operates based on a load factor demand law. This means that the system automatically adjusts the pitch control in relation to the load factor – essentially, it seeks to maintain a specific level of aerodynamic performance even as flight conditions change.

In normal law, when the pilot commands a certain load factor, the system will ensure that the aircraft can respond accordingly, providing the necessary control inputs to maintain stability. This helps ensure that the aircraft behaves in a predictable manner during various maneuvers or changes in flight conditions.

Other options may suggest features of the pitch control system, but they do not accurately reflect the core characteristic of normal law pitch control, which revolves around load factor demand. For instance, while it is true that pitch trim can be automatic when the autopilot is engaged, this isn't a defining trait of normal law; it's more related to autopilot functionality. Similarly, while the aircraft does work towards maintaining an appropriate angle of attack, the specific mechanism in normal law largely focuses on load factor rather than just pitch and bank control. Furthermore, pitch attitude protection is an essential safety aspect, but it is not the defining characteristic associated with normal