14 CFR 27.399 - Dual control system.

§ 27.399 Dual control system.
Each dual primary flight control system must be designed to withstand the loads that result when pilot forces of 0.75 times those obtained under § 27.395 are applied—
(a) In opposition; and
(b) In the same direction.

Title 14 published on 2015-01-01.

No entries appear in the Federal Register after this date, for 14 CFR Part 27.

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United States Code