- Rudder Control Reversal Conditions
- Date issued
- Office of Primary Responsibility
- AIR-600, Policy and Innovation Division
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.
- AC 25.353-1 (PDF)