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  5. § 29.309
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14 CFR · Part 29

14 CFR § 29.309

Design limitations.

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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 following values and limitations must be established to show compliance with the structural requirements of this subpart:

(a)

The design maximum and design minimum weights.

(b)

The main rotor r.p.m. ranges, power on and power off.

(c)

The maximum forward speeds for each main rotor r.p.m. within the ranges determined under paragraph (b) of this section.

(d)

The maximum rearward and sideward flight speeds.

(e)

The center of gravity limits corresponding to the limitations determined under paragraphs (b), (c), and (d) of this section.

(f)

The rotational speed ratios between each powerplant and each connected rotating component.

(g)

The positive and negative limit maneuvering load factors.

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)