What is a potential consequence of exceeding the load factor limits?

Exceeding the load factor limits can lead to structural failure of the wing because aircraft are designed to withstand specific loads during maneuvers, including turns, climbs, and descents. The load factor is a measure of the forces acting on an aircraft relative to its weight, and going beyond the specified limits can result in excessive stress on the aircraft's structure. For instance, during sharp turns or abrupt maneuvers, the load factor increases, which can lead to deformation or failure of critical components, such as wings or fuselage. This is why aircraft specifications include load factor limits to ensure safe operation and maintain the integrity of the aircraft's structure.

The other options do not accurately reflect the consequences of exceeding load factor limits. Increased fuel efficiency, increased range, and improved stability are not outcomes associated with exceeding these limits; in fact, they often relate to proper weight management and adherence to operational limits.