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CS-VLA 351 Yawing conditions
Available versions for ERULES-1963177438-8059
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 351 Yawing conditions ED Decision 2003/18/RM The aeroplane must be designed for yawing loads on the vertical tail surfaces resulting from the loads specified in [CS-VLA 441](#_DxCrossRefBm584936689) to [445](#_DxCrossRefBm584936688).