Center Of Gravity Of An Aircraft
The center of gravity (CG) of an aircraft is the point at which the aircraft would balance if it were possible to suspend it at that point. It is the theoretical point at which the entire weight of the aircraft is assumed to be concentrated. Its position is calculated after supporting the aircraft on at least two sets of weighing scales or load cells, and noting the weight shown on each set of scales or load cell. The center of gravity affects the stability of the aircraft. To ensure the aircraft is safe to fly, the center of gravity must fall within specified limits established by the aircraft manufacturer.
Read more about Center Of Gravity Of An Aircraft: Terminology, Calculation, Incorrect Weight and Balance in Fixed-wing Aircraft, Incorrect Weight and Balance in Helicopters, Lateral Balance, Fuel Dumping and Overweight Operations
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