The three basic quantities

Weight is the load. Arm is its distance from the reference datum. Moment is the turning effect created by that weight at that arm.

Moment = Weight × Arm
Center of gravity = Total moment ÷ Total weight

Use a disciplined table

List every item in the same units, calculate each moment, and total the weight and moment columns separately. Only then calculate center of gravity. If the loading changes, work with the change instead of rebuilding the entire problem when the data permits.

Adding or removing weight

Adding weight moves the center of gravity toward the added item. Removing weight moves it away from the removed item. This directional check can reveal an arithmetic error before the final answer is accepted.

Moving weight

When a load is moved inside the aircraft, total weight does not change. The change in moment depends on the weight moved and the distance moved.

Change in moment = Weight moved × Distance moved

Operational meaning

An excessively forward center of gravity can increase control forces and reduce the ability to rotate or flare. An excessively aft center of gravity can reduce longitudinal stability and make stall recovery more difficult. Total weight also affects takeoff distance, climb, ceiling, landing distance, and structural margins.

Final check: Confirm both total weight and center-of-gravity limits for the relevant phase of flight using approved aircraft data.