Describe the ideal position for an aircraft's center of gravity (CG).

The ideal position for an aircraft's center of gravity (CG) is that it should be within specified limits for safe flight and stability. This positioning is critical because it affects the aircraft's handling characteristics, stability, and overall performance.

When the CG is within the prescribed limits, the aircraft achieves a good balance between controllability and stability. If the CG is too far forward, the aircraft may become overly stable, making it harder to maneuver. Conversely, if it's too far aft, the aircraft can become uncontrollable, especially during maneuvers, leading to a risk of stalling or uncontrollable pitching.

These specified limits are defined in the aircraft's Pilot Operating Handbook (POH) and account for various factors, including the aircraft’s weight and loading configuration. Understanding these limits helps pilots maintain safe operational conditions throughout the flight, from takeoff to landing.

While it might be tempting to think the CG could simply be anywhere in the fuselage, this is not true, as such a position could lead to dangerous flight characteristics. The leading edge of the wing or aft of the wing are also not ideal for achieving the necessary stability for safe flight, as they would be outside of the specified limits. Thus, maintaining the CG within the specified limits is essential