§23.2215. Flight load conditions.

14 C.F.R. § 23.2215

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.

Notes, amendments, and revision history

Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704, Pub. L. 113-53, 127 Stat. 584 (49 U.S.C. 44704) note.

Source: Doc. No. FAA-2015-1621, Amdt. 23-64, 81 FR 96689, Dec. 30, 2016, unless otherwise noted.