14 CFR 25.405

§ 25.405 Secondary control system.

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

Cite this

Citation: 14 CFR 25.405, § 25.405 Secondary control system, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54037
Permanent ID: ys:prov:54037@1
SHA-256: f83b1b4677e7dd889445d7fdf4d843c802509576a5968594841ace905066008b

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Full text

Secondary controls, such as wheel brake, spoiler, and tab controls, must be designed for the maximum forces that a pilot is likely to apply to those controls. The following values may be used: Pilot Control Force Limits (Secondary Controls)

Legislative history

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