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CS-VLA 29 Empty weight and corresponding centre of gravity
Available versions for ERULES-1963177438-7832
ED Decision 2003/18/RM
found in: CS-VLA Amdt 1 - Very Light Aeroplanes (Mar 2009)
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CS-VLA Amdt 1 - Ve... (Mar 2009)
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CS-VLA 29 Empty weight and corresponding centre of gravity ED Decision 2003/18/RM (a) The empty weight and corresponding centre of gravity must be determined by weighing the aeroplane with - (1) Fixed ballast; (2) Unusable fuel determined under [CS-VLA 959](#_DxCrossRefBm584936621); and (3) Full operating fluids, including - (i) Oil; (ii) Hydraulic fluid; and (iii) Other fluids required for operation of aeroplane systems, (b) The condition of the aeroplane at the time of determining empty weight must be one that is well defined and can be easily repeated.