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AMC VLA 572(a) Parts of structure critical to safety (Interpretative Material)
Available versions for ERULES-1963177438-7890
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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AMC VLA 572(a) Parts of structure critical to safety (Interpretative Material) ED Decision 2003/18/RM At least the wing main spar, the horizontal tail and their attachments to the fuselage should be investigated to determine whether or not their stress levels exceed the values given in the table in [AMC VLA 572(b)](#_DxCrossRefBm584936740).