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.
- Content
-
- AC 25.353-1 (PDF)