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(a) The airplane must be designed for the symmetrical maneuvers prescribed in Sec. Sec. 25.333 and 25.337, the yawing maneuvers in Sec. 25.351, and the vertical and lateral gust and turbulence conditions prescribed in Sec. 25.341(a) and (b) at each setting and the maximum speed associated with that setting; and
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Control Surface and System Loads