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  5. § 29.751
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14 CFR · Part 29

14 CFR § 29.751

Main float buoyancy.

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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 main floats, the buoyancy necessary to support the maximum weight of the rotorcraft in fresh water must be exceeded by—

(1)

50 percent, for single floats; and

(2)

60 percent, for multiple floats.

(b)

Each main float must have enough water-tight compartments so that, with any single main float compartment flooded, the mainfloats will provide a margin of positive stability great enough to minimize the probability of capsizing.

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)