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Part 29
§ 29.629

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14 CFR · Part 29

14 CFR § 29.629

Flutter and divergence.

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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

Each aerodynamic surface of the rotorcraft must be free from flutter and divergence under each appropriate speed and power condition.

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)