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  5. § 23.2230
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14 CFR · Part 23

14 CFR § 23.2230

Limit and ultimate loads.

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Read in Subpart C
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

The applicant must determine—

(a)

The limit loads, which are equal to the structural design loads unless otherwise specified elsewhere in this part; and

(b)

The ultimate loads, which are equal to the limit loads multiplied by a 1.5 factor of safety unless otherwise specified elsewhere in this part.

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)