ED Decision 2003/16/RM
Each auxiliary lifting surface must be designed to withstand:
(a) The critical flight loads in CS 29.337 to 29.341, and CS 29.351;
(b) The applicable ground loads in CS 29.235, 29.471 to 29.485, CS 29.493, 29.505, and 29.521; and
(c) Any other critical condition expected in normal operation.
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