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With the table method, the CG position is determined by dividing the total moments by the total weight. As weights are shifted around within the airplane by moving baggage from forward to aft compartments, moving passengers, or even extending and retracting the landing gear, the CG will follow.
The oil must either be drained before the aircraft is weighed, or its weight must be subtracted from the scale readings to determine the empty weight.
The weight and balance system commonly employed among aircraft consists of three equally important elements: the weighing of the aircraft, the maintaining of the weight and balance records, and the proper loading of the aircraft.
The total weight W of the aircraft is simply the sum of the weight of all of the individual components. W = w(fuselage) + w(wing) + w(engines) + w(payload) + w(fuel) + ...
With the table method, the CG position is determined by dividing the total moments by the total weight. As weights are shifted around within the airplane by moving baggage from forward to aft compartments, moving passengers, or even extending and retracting the landing gear, the CG will follow.
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Ascertain from the pilot's operating handbook the empty weight of the aircraft and determine the weights of people, baggage, and fuel. Multiply each weight by the arm\u2014the distance from the reference datum\u2014to find the moment. Add all the weights to find the gross weight. Add all the moments to find the total moment.
Technique: Weight and balance Ascertain from the pilot's operating handbook the empty weight of the aircraft and determine the weights of people, baggage, and fuel. Multiply each weight by the arm\u2014the distance from the reference datum\u2014to find the moment. Add all the weights to find the gross weight.
Usually it's on the airplane's nose (point of the spinner) or the leading edge of the wings. Station\u2014A location along the aircraft fuselage, usually measured in inches from the datum. Useful Load\u2014The difference between the aircraft's empty and maximum weight.
The total weight W of the aircraft is simply the sum of the weight of all of the individual components. W = w(fuselage) + w(wing) + w(engines) + w(payload) + w(fuel) + ...
Technique: Weight and balance Ascertain from the pilot's operating handbook the empty weight of the aircraft and determine the weights of people, baggage, and fuel. Multiply each weight by the arm\u2014the distance from the reference datum\u2014to find the moment. Add all the weights to find the gross weight.

blank aircraft weight and balance revision form