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DOT/FAA RIN: 2120-AJ56 Publication ID: Spring 2011 
Title: Function and Reliability Testing for Turbine-powered Airplanes Less than 6,000 Pounds 
Abstract: This rulemaking would amend the flight test requirements to include function and reliability testing for turbine-powered airplanes that are less than 6,000 pounds. These requirements would address technological advancements in airplane structure, equipment and materials used in new airplanes. These requirements would ensure that the airplane and its components and equipment are reliable and function properly. 
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 21   
Legal Authority: 42 USC 7572    49 USC 106(g)    49 USC 40105    49 USC 40113    49 USC 44701 to 44702    49 USC 44704    49 USC 44707    49 USC 44709    49 USC 44711    49 USC 44713    49 USC 44715    49 USC 45303   
Legal Deadline:
Action Source Description Date
Final  Statutory  Final Rule  11/08/2011 
Timetable:
Action Date FR Cite
NPRM  04/09/2010  75 FR 18134   
NPRM Comment Period End  07/08/2010    
Final Rule  09/00/2011    
Additional Information: This rule will provide a cost savings.
Regulatory Flexibility Analysis Required: No  Government Levels Affected: None 
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:
Victor Powell
Department of Transportation
Federal Aviation Administration
950 L'Enfant Plaza,
Washington, DC 20591
Phone:202-385-6326
Email: victor.powell@faa.gov