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DOT/FAA RIN: 2120-AK89 Publication ID: Spring 2019 
Title: Yaw Maneuver Conditions--Rudder Reversals (Formerly Vertical Stabilizer Loads for Transport Category Airplanes) 
Abstract:

This rulemaking would incorporate a new load condition into part 25. The new load condition would be a performance-based rule that 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 
EO 13771 Designation: Fully or Partially Exempt 
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
Timetable:
Action Date FR Cite
NPRM  07/16/2018  83 FR 32807   
NPRM Comment Period End  10/15/2018 
NPRM Comment Period End  10/15/2018 
Final Rule  01/00/2020 
Regulatory Flexibility Analysis Required: No  Government Levels Affected: Undetermined 
Small Entities Affected: No  Federalism: No 
Included in the Regulatory Plan: No 
RIN Information URL: www.regulations.gov   Public Comment URL: www.regulations.gov  
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
Phone:206-231-3182
Email: robert.c.jones@faa.gov