What are the limit load factors for the Utility category with flaps up?

In the Utility category, limit load factors are defined to ensure that the aircraft can withstand certain levels of stress during normal operations without experiencing structural failure. For aircraft in the Utility category, the limit load factors with flaps up are +4.0g for positive load factors and -1.5g for negative load factors.

This classification of load factors is crucial because it determines the aircraft's capability to handle maneuvers such as turns, climbs, and descents without overstressing the airframe. The positive load factor signifies the maximum amount of "g forces" that can be safely exerted during flight, while the negative load factor indicates the maximum force the aircraft can handle in the opposite direction. Specifically, a +4.0g limit allows for safe aerobatic and operational maneuvers within the confines of the Utility category, which is designed for more versatile use than the Light Sport or Normal categories, providing the pilot with a greater degree of maneuverability and safety.

Also, the other options present limits that exceed what is established for the Utility category. Each of these reflects load factors from different categories of aircraft or suggest scenarios that are not typical for this classification. Hence, the correct representation of limit load factors for the Utility category with flaps