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Federal Aviation Regulation Sec. 23.45 - General.
Home > Aviation Regulations > Parts Index > Part 23 > Sec. 23.45 - General.
Sec. 23.45 — General.
(3) For reciprocating engine-powered airplanes of more than 6,000 pounds maximum weight and turbine engine-powered airplanes, temperature from standard to 30 °C above standard, or the maximum ambient atmospheric temperature at which compliance with the cooling provisions of §23.1041 to §23.1047 is shown, if lower.
(c) Performance data must be determined with the cowl flaps or other means for controlling the engine cooling air supply in the position used in the cooling tests required by §23.1041 to §23.1047.
(1) Takeoff distance of §23.53(b);
(2) Accelerate-stop distance of §23.55;
(3) Takeoff distance and takeoff run of §23.59; and
(4) Landing distance of §23.75.
Note: The effect on these distances of operation on other types of surfaces (for example, grass, gravel) when dry, may be determined or derived and these surfaces listed in the Airplane Flight Manual in accordance with §23.1583(p).
(4) Procedures for the execution of discontinued approaches and balked landings associated with the conditions prescribed in §23.67(c)(4) and §23.77(c) must be established.
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