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§ 23.2125 - Climb information.

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The applicant must determine climb performance at each weight, altitude, and ambient temperature within the operating limitations—

For all single-engine airplanes;

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

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.

The applicant must determine the glide performance for single-engine airplanes after a complete loss of thrust.

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§ 23.2120 - Climb requirements.
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§ 23.2130 - Landing.