§ 23.2215. Flight load conditions.
47 words·~1 min read·
/us/cfr/t14/s§ 23.2215·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
The applicant must determine the structural design loads resulting from the following flight conditions:
(a)Atmospheric gusts where the magnitude and gradient of these gusts are based on measured gust statistics.
(b)Symmetric and asymmetric maneuvers.
(c)Asymmetric thrust resulting from the failure of a powerplant unit.