If load distribution causes the center of gravity to exceed limits, what is the most likely consequence?

• A. Degrades handling and performance
• B. Faster engine response
• C. Longer wheelbase
• D. Increase in cabin pressurization

Answer: (A)

Center of gravity location governs longitudinal stability and how effectively the airplane can be controlled. When load distribution pushes the CG outside the approved range, the aircraft becomes harder to manage and its performance envelope narrows. A forward CG increases nose-down tendency, raises stall speed, and reduces elevator authority and trim effectiveness; an aft CG reduces stability and can lead to overcontrol and less predictable pitch behavior. In either case, handling quality and overall performance degrade, making maneuvers less precise and increasing the risk during critical phases like takeoff and landing. The other options don’t reflect how CG placement influences flight characteristics—engine response is driven by propulsion, wheelbase is fixed, and cabin pressurization is a separate system.