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  5. § 27.753
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14 CFR · Part 27

14 CFR § 27.753

Main float design.

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Read in Subpart D
Part 27 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 27: Instructions for Continued Airworthiness
  • Appendix B to Part 27: Airworthiness Criteria for Helicopter Instrument Flight
  • Appendix C to Part 27: Criteria for Category A
  • Appendix D to Part 27: HIRF Environments and Equipment HIRF Test Levels
(a)

Bag floats. Each bag float must be designed to withstand—

(1)

The maximum pressure differential that might be developed at the maximum altitude for which certification with that float is requested; and

(2)

The vertical loads prescribed in § 27.521(a), distributed along the length of the bag over three-quarters of its projected area.

(b)

Rigid floats. Each rigid float must be able to withstand the vertical, horizontal, and side loads prescribed in § 27.521. These loads may be distributed along the length of the float.

Regulations Referenced

14 CFR 27.521

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 27)