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  5. § 29.361
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14 CFR · Part 29

14 CFR § 29.361

Engine torque.

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Read in Subpart C
Part 29 Contents
  • Subpart A: General
  • Subpart B: Flight
  • Subpart C: Strength Requirements
  • Subpart D: Design and Construction
  • Subpart E: Powerplant
  • Subpart F: Equipment
  • Subpart G: Operating Limitations and Information
  • Appendix A to Part 29: Instructions for Continued Airworthiness
  • Appendix B to Part 29: Airworthiness Criteria for Helicopter Instrument Flight
  • Appendix C to Part 29: Icing Certification
  • Appendix D to Part 29: Criteria for Demonstration of Emergency Evacuation Procedures Under § 29.803
  • Appendix E to Part 29: HIRF Environments and Equipment HIRF Test Levels

The limit engine torque may not be less than the following:

(a)

For turbine engines, the highest of—

(1)

The mean torque for maximum continuous power multiplied by 1.25;

(2)

The torque required by § 29.923;

(3)

The torque required by § 29.927; or

(4)

The torque imposed by sudden engine stoppage due to malfunction or structural failure (such as compressor jamming).

(b)

For reciprocating engines, the mean torque for maximum continuous power multiplied by—

(1)

1.33, for engines with five or more cylinders; and

(2)

Two, three, and four, for engines with four, three, and two cylinders, respectively.

Regulations Referenced

14 CFR 29.92314 CFR 29.927

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 29)