14 CFR · Part 23
14 CFR § 23.2215
Flight load conditions.
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.
Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.
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