Code of Federal Regulations (Last Updated: November 8, 2024) |
Title 14 - Aeronautics and Space |
Chapter I - Federal Aviation Administration, Department of Transportation |
SubChapter C - Aircraft |
Part 23 - Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes |
Subpart B - Flight |
Controllability and Maneuverability |
§ 23.153 - Control during landings.
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§ 23.153 Control during landings.
It must be possible, while in the landing configuration, to safely complete a landing without exceeding the one-hand control force limits specified in § 23.143(c) following an approach to land -
(a) At a speed of VREF minus 5 knots;
(b) With the airplane in trim, or as nearly as possible in trim and without the trimming control being moved throughout the maneuver;
(c) At an approach gradient equal to the steepest used in the landing distance demonstration of § 23.75; and
(d) With only those power changes, if any, that would be made when landing normally from an approach at VREF.
[Doc. No. 27807, 61 FR 5189, Feb. 9, 1996]