Directional and lateral control.

CFR · 2024-01-01 · US · Title 14

(a) (1) The critical engine inoperative and its propeller in the minimum drag position; (2) The power required for level flight at 1.3 (3) The most unfavorable center of gravity; (4) Landing gear retracted; (5) Flaps in the approach position; and (6) Maximum landing weight. (b) (1) The two critical engines must be inoperative with their propellers (if applicable) in the minimum drag position; (2) [Reserved] (3) The flaps must be in the most favorable climb position. (c) (1) The critical engine inoperative and its propeller (if applicable) in the minimum drag position; (2) The remaining engines at maximum continuous power; (3) The most unfavorable center of gravity; (4) Landing gear (i) retracted and (ii) extended; (5) Flaps in the most favorable climb position; and (6) Maximum takeoff weight. (d) (e) (f)

official document · source cfr-2024 · id 14:§ 25.147