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Code · CFR · Title 14 — Aeronautics and Space · Part 23 — Airworthiness Standards: Normal Category Airplanes · § 23.2300

§ 23.2300. Flight control systems.

100 words·~1 min read·/us/cfr/t14/s§ 23.2300·

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(a)The applicant must design airplane flight control systems to:
(1)Operate easily, smoothly, and positively enough to allow proper performance of their functions.
(2)Protect against likely hazards.
(b)The applicant must design trim systems, if installed, to:
(1)Protect against inadvertent, incorrect, or abrupt trim operation.
(2)Provide a means to indicate—
(i)The direction of trim control movement relative to airplane motion;
(ii)The trim position with respect to the trim range;
(iii)The neutral position for lateral and directional trim; and
(iv)The range for takeoff for all applicant requested center of gravity ranges and configurations.
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