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  5. § 29.1145
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14 CFR · Part 29

14 CFR § 29.1145

Ignition switches.

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Read in Subpart E
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
(a)

Ignition switches must control each ignition circuit on each engine.

(b)

There must be means to quickly shut off all ignition by the grouping of switches or by a master ignition control.

(c)

Each group of ignition switches, except ignition switches for turbine engines for which continuous ignition is not required, and each master ignition control must have a means to prevent its inadvertent operation.

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)