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DOT/FAA | RIN: 2120-AJ56 | Publication ID: Fall 2010 |
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 49 USC 44702 49 USC 44704 49 USC 44707 49 USC 44709 49 USC 44711 49 USC 44713 49 USC 44715 49 USC 45303 |
Legal Deadline:
None |
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Timetable:
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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 |