RV14Awb
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ARMS Fuel………………………81.97 inches aft of datum Pilot & Passenger………99.83” aft of datum Baggage…………………129.48” aft of datum (center of baggage area) DETERMINING EMPTY CG Level the aircraft longitudinally and laterally using the longerons in the cabin area as the level reference. Weigh the airplane with the canopy closed, full oil and the fuel tanks empty. Enter the weights and distances from the datum (arm) in the chart below. Multiply weight by arm to obtain moment. Divide the total moment by the weight to determine the empty CG. Weight Right Wheel Left Wheel Nose Wheel Total CG

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