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  5. § 135.398
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14 CFR · Part 135

14 CFR § 135.398

Commuter category airplanes performance operating 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 may operate a commuter category airplane unless that person complies with the takeoff weight limitations in the approved Airplane Flight Manual.

(b)

No person may take off an airplane type certificated in the commuter category at a weight greater than that listed in the Airplane Flight Manual that allows a net takeoff flight path that clears all obstacles either by a height of at least 35 feet vertically, or at least 200 feet horizontally within the airport boundaries and by at least 300 feet horizontally after passing the boundaries.

(c)

No person may operate a commuter category airplane unless that person complies with the landing limitations prescribed in §§ 135.385 and 135.387 of this part. For purposes of this paragraph, §§ 135.385 and 135.387 are applicable to all commuter category airplanes notwithstanding their stated applicability to turbine-engine-powered large transport category airplanes.

(d)

In determining maximum weights, minimum distances and flight paths under paragraphs (a) through (c) of this section, correction must be made for the runway to be used, the elevation of the airport, the effective runway gradient, and ambient temperature, and wind component at the time of takeoff.

(e)

For the purposes of this section, the assumption is that the airplane is not banked before reaching a height of 50 feet as shown by the net takeoff flight path data in the Airplane Flight Manual and thereafter the maximum bank is not more than 15 degrees.

Regulations Referenced

14 CFR 135.38514 CFR 135.387

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)