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14 CFR · Part 135

14 CFR § 135.367

Large transport category airplanes: Reciprocating engine powered: Takeoff limitations.

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Read in Subpart I
Part 135 Contents
  • Subpart A: General
  • Subpart B: Flight Operations
  • Subpart C: Aircraft and Equipment
  • Subpart D: VFR/IFR Operating Limitations and Weather Requirements
  • Subpart E: Flight Crewmember Requirements
  • Subpart F: Crewmember Flight Time and Duty Period Limitations and Rest Requirements
  • Subpart G: Crewmember Testing Requirements
  • Subpart H: Training
  • Subpart I: Airplane Performance Operating Limitations
  • Subpart J: Maintenance, Preventive Maintenance, and Alterations
  • Subpart K: Hazardous Materials Training Program
  • Subpart L: Helicopter Air Ambulance Equipment, Operations, and Training Requirements
  • Appendix A to Part 135: Additional Airworthiness Standards for 10 or More Passenger Airplanes
  • Appendix B to Part 135: Airplane Flight Recorder Specifications
  • Appendix C to Part 135: Helicopter Flight Recorder Specifications
  • Appendix D to Part 135: Airplane Flight Recorder Specification
  • Appendix E to Part 135: Helicopter Flight Recorder Specifications
  • Appendix F to Part 135: Airplane Flight Recorder Specification
  • Appendix G to Part 135: Extended Operations (ETOPS)
(a)

No person operating a reciprocating engine powered large transport category airplane may take off that airplane unless it is possible—

(1)

To stop the airplane safely on the runway, as shown by the accelerate-stop distance data, at any time during takeoff until reaching critical-engine failure speed;

(2)

If the critical engine fails at any time after the airplane reaches critical-engine failure speed V1, to continue the takeoff and reach a height of 50 feet, as indicated by the takeoff path data, before passing over the end of the runway; and

(3)

To clear all obstacles either by at least 50 feet vertically (as shown by the takeoff path data) or 200 feet horizontally within the airport boundaries and 300 feet horizontally beyond the boundaries, without banking before reaching a height of 50 feet (as shown by the takeoff path data) and after that without banking more than 15 degrees.

(b)

In applying this section, corrections must be made for any runway gradient. To allow for wind effect, takeoff data based on still air may be corrected by taking into account not more than 50 percent of any reported headwind component and not less than 150 percent of any reported tailwind component.

Referenced By

Interpretations of This Section (1)

  • Morris, 2008

Documents that cite this section, found in their catalog metadata or text. Listed by date, not by significance.

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 135)