Landing.

CFR · 2024-01-01 · US · Title 14

(a) The horizontal distance necessary to land and to come to a complete stop (or to a speed of approximately 3 knots for water landings) from a point 50 feet above the landing surface must be determined (for standard temperatures, at each weight, altitude, and wind within the operational limits established by the applicant for the airplane): (1) In non-icing conditions; and (2) In icing conditions with the most critical of the landing ice accretion(s) defined in Appendices C and O of this part, as applicable, in accordance with § 25.21(g), if V (b) In determining the distance in paragraph (a) of this section: (1) The airplane must be in the landing configuration. (2) A stabilized approach, with a calibrated airspeed of not less than V (i) In non-icing conditions, V (A) 1.23 V (B) V (C) A speed that provides the maneuvering capability specified in § 25.143(h). (ii) In icing conditions, V (A) The speed determined in paragraph (b)(2)(i) of this section; (B) 1.23 V (C) A speed that provides the maneuvering capability specified in § 25.143(h) with the most critical of the landing ice accretion(s) defined in Appendices C and O of this part, as applicable, in accordance with § 25.21(g). (3) Changes in configuration, power or thrust, and speed, must be made in accordance with the established procedures for service operation. (4) The landing must be made without excessive vertical acceleration, tendency to bounce, nose over, ground loop, porpoise, or water loop. (5) The landings may n

official document · source cfr-2024 · id 14:§ 25.125