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CS-VLA 23 Load distribution limits
Available versions for ERULES-1963177438-8089
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 23 Load distribution limits ED Decision 2003/18/RM Ranges of weight and centres of gravity within which the aeroplane may be safely operated must be established and must include the range of lateral centres of gravity if possible loading conditions can result in significant variation of their positions.