Flight load conditions.

CFR · 2024-01-01 · US · Title 14

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.

official document · source cfr-2024 · id 14:§ 23.2215