§ 23.2125. Climb information.
94 words·~1 min read·
/us/cfr/t14/s§ 23.2125·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
(a)The applicant must determine climb performance at each weight, altitude, and ambient temperature within the operating limitations—
(1)For all single-engine airplanes;
(2)For levels 1 and 2 high-speed multiengine airplanes and level 3 multiengine airplanes, following a critical loss of thrust on takeoff in the initial climb configuration; and
(3)For all multiengine airplanes, during the enroute phase of flight with all engines operating and after a critical loss of thrust in the cruise configuration.
(b)The applicant must determine the glide performance for single-engine airplanes after a complete loss of thrust.