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  5. § 23.2420
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14 CFR · Part 23

14 CFR § 23.2420

Reversing systems.

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Read in Subpart E
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

Each reversing system must be designed so that—

(a)

No unsafe condition will result during normal operation of the system; and

(b)

The airplane is capable of continued safe flight and landing after any single failure, likely combination of failures, or malfunction of the reversing system.

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)