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Code · CFR · Title 14 — Aeronautics and Space · Part 29 — Airworthiness Standards: Transport Category Rotorcraft · § 29.753

§ 29.753. Main float design.

85 words·~1 min read·/us/cfr/t14/s§ 29.753·

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(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 § 29.521(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 § 29.521. An appropriate load distribution under critical conditions must be used.
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