Skip to Main Content
FlightPushFLIGHTPUSH
Part 23

Learn

Dashboard My Courses Mastery Map Practice Flight Bag

Resources

CFR & AIM FAA Orders Handbooks & Guides Certification Standards Pilot/Controller Glossary Advisory Circulars Legal Interpretations
Safety Center
Articles Trust Center
Help Center FAQ Status
  1. Reference Library
  2. CFR & AIM
  3. CFR
  4. Part 23
  5. § 23.2115
Loading
flightpush.co home

14 CFR · Part 23

14 CFR § 23.2115

Takeoff performance.

← Previous SectionNext Section →
Read in Subpart B
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 determine airplane takeoff performance accounting for—

(1)

Stall speed safety margins;

(2)

Minimum control speeds; and

(3)

Climb gradients.

(b)

For single engine airplanes and levels 1, 2, and 3 low-speed multiengine airplanes, takeoff performance includes the determination of ground roll and initial climb distance to 50 feet (15 meters) above the takeoff surface.

(c)

For levels 1, 2, and 3 high-speed multiengine airplanes, and level 4 multiengine airplanes, takeoff performance includes a determination of the following distances after a sudden critical loss of thrust—

(1)

An aborted takeoff at critical speed;

(2)

Ground roll and initial climb to 35 feet (11 meters) above the takeoff surface; and

(3)

Net takeoff flight path.

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)