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DOT/FAA RIN: 2120-AK89 Publication ID: Fall 2022 
Title: Yaw Maneuver Conditions--Rudder Reversals 

This rulemaking would incorporate a new load condition into 14 CFR part 25. The new load condition would be performance-based and would require applicants to demonstrate the integrity of the airplane structure, including its vertical stabilizer(fin), in the presence of pilot-commanded rudder pedal reversals. Adopting the new load condition would protect the airplane from excessive loads on the vertical stabilizer due to pilot-commanded rudder pedal reversals.

Agency: Department of Transportation(DOT)  Priority: Substantive, Nonsignificant 
RIN Status: Previously published in the Unified Agenda Agenda Stage of Rulemaking: Final Rule Stage 
Major: No  Unfunded Mandates: No 
CFR Citation: 14 CFR 25   
Legal Authority: 49 U.S.C. 106(f)    49 U.S.C. 44701(a)    49 U.S.C. 44702    49 U.S.C. 44704(a)   
Legal Deadline:  None
Action Date FR Cite
NPRM  07/16/2018  83 FR 32807   
NPRM Comment Period End  10/15/2018 
Analyzing Comments  06/03/2019 
Final Rule  12/00/2022 
Regulatory Flexibility Analysis Required: No  Government Levels Affected: Undetermined 
Small Entities Affected: No  Federalism: No 
Included in the Regulatory Plan: No 
RIN Information URL:   Public Comment URL:  
RIN Data Printed in the FR: No 
Agency Contact:
Robert Jones
Department of Transportation
Federal Aviation Administration
200 S 216th Street,
Des Moines, WA 98198