Climb information.

CFR · 2024-01-01 · US · Title 14

(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.

official document · source cfr-2024 · id 14:§ 23.2125