ED Decision 2003/18/RM
(a) The design load criteria in this Appendix are an approved equivalent of those in CS-VLA 321 to 459 of this document for the certification of conventional very light aeroplanes as defined in CS-VLA 1 and 301(d) and AMC 301(d).
(b) Unless otherwise stated, the nomenclature and symbols in this Appendix are the same as the corresponding nomenclature and symbols in CS-VLA.
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