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Part 29
§ 29.181

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14 CFR · Part 29

14 CFR § 29.181

Dynamic stability: Category A rotorcraft.

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Read in Subpart B

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

Any short-period oscillation occurring at any speed from VY to VNE must be positively damped with the primary flight controls free and in a fixed position.

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)