Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information 4.5 Calculation Example The following example is given to show how to calculate the center of gravity „CG“. Weight lb Arm Inch Moment lb-Inch Empty Weight 670 12.5* 8,375 Occupants 175 8.3 1,452.5 Fuel 120 37.8 4,536 Baggage 30 37.4 1,122 Weight Total: 995 Moment Total: 15,485.5 Center of Gravity (Inch) = Moment Total (lb-Inch) Weight Total (lb) = 15,56 Inch Calculation example to determine payload In the example below the maximum take-off weight is 1,320 lb at an empty weight of 670 lb. A. Fuel quantity 10 gallons = 60 lb Permissible payload: = 590 lb B. Fuel quantity 20 gallons = 120 lb Permissible payload: = 530 lb Weight and Balance Information 4 - 5
Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information 4.6 CG-Diagram 4.7 Aircraft Specific Weights Below the aircraft specific data shall be notified. Pilots must use this information to ensure a correct weight and balance calculation prior to every flight. This is essential for a safe conduction of each flight. Empty Weight: lb Maximum Take-Off Weight: lb Maximum Payload: lb Center of Grafity „CG“: inches behind R.P. Weight and Balance Information 4 - 6
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Pilot Operating Handbook - Ecoflight.ch

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