Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information 4.3 Center of Gravity Range and Determination To determine “CG”, put the aircraft on 3 weighing scales, positioned on a level surface. Before weighing, a level wing main chord has to be established (use pads between main wheels and scale beneath). A check-mark (R.P.) on the leading edge of the left wing, adjacent to the wing root is provided to ease examination to level wing main chord - use a flexible clear hose, filled with water as a spirit level. The total weight G = G1 + G2, has to be used for calculating “CG”, located at the distance “X” behind R.P. Weight and Balance Information 4 - 3
Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information 4.4 CG-Calculation The following procedure has to be maintained for the correct calculation of the center of gravity “CG”. Moment (lb-Inch) = Weight (lb) x Arm (Inch) Center of Gravity (Inch) = Moment Total (lb-Inch) Weight Total (lb) Weight lb Arm Inch Moment lb-Inch Empty Weight ____ ____ ____ Occupants ____ 8.3 ____ Fuel ____ 37.8 ____ Baggage ____ 37.4 ____ Weight Total: ____ Moment Total: ____ The permissible CG range, measured from R.P. must be within the limits of 9.6 to 16.3 Inches. Weight and Balance Information 4 - 4
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Page 3 and 4: Rev. 02 - July 16 th , 2009 Introdu
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Rev. 02 - July 16 th , 2009 Imprint
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