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DOT/FAA

RIN: 2120-AK89

Publication ID: Fall 2022

Title: Yaw Maneuver Conditions--Rudder Reversals
Abstract: 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

Timetable:

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: 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