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United States Department of Transportation United States Department of Transportation

AC 25.353-1 - Rudder Control Reversal Conditions

Document Information

Number
25.353-1
Title
Rudder Control Reversal Conditions
Status
Active
Date issued
2022-11-28
Office of Primary Responsibility
AIR-600, Policy and Innovation Division
Description

This AC describes acceptable means for showing compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) 25.353, Rudder control reversal conditions, at amendment 25-147. Section 25.353 requires that transport category airplanes be designed to withstand the structural load conditions that result from at least three cyclic, full rudder pedal reversals, if those airplanes have a powered rudder control surface or surfaces.

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