What is a primary consequence of a tail-heavy condition?

A tail-heavy condition significantly impacts the aircraft's stability and control during flight. When an aircraft is tail-heavy, its center of gravity shifts towards the tail section, which can lead to difficulty in recovering from a stall. In this condition, the aircraft may have a tendency to pitch up excessively, increasing the risk of a stall, and making it challenging to regain control.

During a stall, the aerodynamic forces that allow for recovery are compromised. A tail-heavy aircraft can also have a higher angle of attack at which the stall occurs, leading to a more abrupt loss of lift. This compromised stability makes effective recovery from a stall more difficult, increasing the potential for an accident.

Other choices relate to aspects that would not be enhanced or improved in a tail-heavy condition. For instance, control at low speeds typically requires a more balanced center of gravity for effective handling, while features such as nose wheel steering and flight efficiency are not positively impacted. In fact, they can suffer due to the adverse effects of a tail-heavy load, reinforcing the importance of maintaining proper weight distribution in aircraft operation.