What is the maximum load factor during normal flight for the CRJ 200?

The correct answer reflects the aircraft's design limitations regarding load factors during normal flight. For the CRJ 200, the maximum load factor is indeed +2.5g in positive loading conditions and -1.0g in negative loading conditions.

This range is established to ensure structural integrity and safety under various flight maneuvers and conditions, particularly during turbulent encounters or when sharp turns are executed. The positive limit allows for a margin that supports increased load during maneuvers, such as climbing or during turbulence, while the negative limit indicates the maximum safe deviation in the opposite direction.

Understanding these limits is crucial for pilots to maintain safe operation, ensuring that the aircraft operates within its structural design parameters. The other options present incorrectly higher negative load factors or unattainable positive limits that do not align with the aircraft's operational specifications as outlined in the manufacturer's documentation.