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  5. § 29.805
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14 CFR · Part 29

14 CFR § 29.805

Flight crew emergency exits.

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Read in Subpart D
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)

For rotorcraft with passenger emergency exits that are not convenient to the flight crew, there must be flight crew emergency exits, on both sides of the rotorcraft or as a top hatch, in the flight crew area.

(b)

Each flight crew emergency exit must be of sufficient size and must be located so as to allow rapid evacuation of the flight crew. This must be shown by test.

(c)

Each exit must not be obstructed by water or flotation devices after a ditching. This must be shown by test, demonstration, or analysis.

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)