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Final Rule

Document ID: FAA-1999-5835-0010
Document Type: Rule
Agency: Federal Aviation Administration
Topics: No Topics associated with this document
CFR Citation: 14 CFR 25
View Document:  View as format pdf

Details Information

Abstract: This amendment revises the airworthiness standards for landing gear shock absorption test requirements for transport category airplanes by incorporating changes developed in cooperation with the Joint Aviation Authorities (JAA) of Europe and the U.S. and European aviation industry through the Aviation Rulemaking Advisory Committee (ARAC). This amendment reduces the number of design weight conditions required to be demonstrated by shock absorption tests and changes the objective of the tests to include the complete validation of the landing gear dynamic characteristics. This amendment also removes some means of compliance criteria from the rule since it is more appropriately set forth in advisory material. EFFECTIVE DATE: June 15, 2001.
Document Subtype: Federal Register Publication
Received Date: May 16 2001, at 12:00 AM Eastern Daylight Time
Page Count: 6
Comment Due Date: May 16 2001, at 11:59 PM Eastern Standard Time

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