Revised Landing Gear Shock Absorption Test Requirements
other · Rule · Final rule. · Published 2001-05-16 · 66 FR 27390
Document
Document number
01-12231
Federal Register citation
66 FR 27390
Type
Rule
Action
Final rule.
Category
other
Publication date
2001-05-16
FAA docket
Docket No. FAA-1999-5835
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.