14 CFR 27.399

§ 27.399 Dual control system.

United States · 14 CFR — Aeronautics and Space · Status: effective

Cite this

Citation: 14 CFR 27.399, § 27.399 Dual control system, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54458
Permanent ID: ys:prov:54458@1
SHA-256: ebff82b0ec11f0c26cf8e730d6184617852f9a91ed1bd595b92856890716074d

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Full text

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.

Legislative history

This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.