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  5. § 23.2300
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14 CFR · Part 23

14 CFR § 23.2300

Flight control systems.

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Read in Subpart D
Part 23 Contents
  • §§ 23.1457–23.1529
  • Subpart A: General
  • Subpart B: Flight
  • Subpart C: Structures
  • Subpart D: Design and Construction
  • Subpart E: Powerplant
  • Subpart F: Equipment
  • Subpart G: Flightcrew Interface and Other Information
  • Appendix A to Part 23: Instructions for Continued Airworthiness
(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.

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 23)