Takeoff speeds.

CFR · 2024-01-01 · US · Title 14

(a) V (1) V (2) V (b) (1) 1.13 (i) Two-engine and three-engine turbopropeller and reciprocating engine powered airplanes; and (ii) Turbojet powered airplanes without provisions for obtaining a significant reduction in the one-engine-inoperative power-on stall speed; (2) 1.08 (i) Turbopropeller and reciprocating engine powered airplanes with more than three engines; and (ii) Turbojet powered airplanes with provisions for obtaining a significant reduction in the one-engine-inoperative power-on stall speed; and (3) 1.10 times (c) (1) V (2) (3) A speed that provides the maneuvering capability specified in § 25.143(h). (d) V (e) (1) (i) (ii) 105 percent of (iii) The speed (determined in accordance with § 25.111(c)(2)) that allows reaching (iv) A speed that, if the airplane is rotated at its maximum practicable rate, will result in a V (A) 110 percent of V (B) If the V (2) For any given set of conditions (such as weight, configuration, and temperature), a single value of (3) It must be shown that the one-engine-inoperative takeoff distance, using a rotation speed of 5 knots less than (4) Reasonably expected variations in service from the established takeoff procedures for the operation of the airplane (such as over-rotation of the airplane and out-of-trim conditions) may not result in unsafe flight characteristics or in marked increases in the scheduled takeoff distances established in accordance with § 25.113(a). (f) (g) (1) 1.18 (2) A speed that provides the maneuvering capabilit

official document · source cfr-2024 · id 14:§ 25.107