Trim.

CFR · 2024-01-01 · US · Title 14

(a) (b) (c) (1) A climb with maximum continuous power at a speed not more than 1.3 (2) Either a glide with power off at a speed not more than 1.3 V (3) Level flight at any speed from 1.3 (d) (1) The critical engine inoperative; (2) The remaining engines at maximum continuous power; and (3) The landing gear and flaps retracted. (e) Airplanes with four or more engines. Each airplane with four or more engines must also maintain trim in rectilinear flight with the most unfavorable center of gravity and at the climb speed, configuration, and power required by § 25.123(a) for the purpose of establishing the en route flight paths with two engines inoperative.

official document · source cfr-2024 · id 14:§ 25.161