Airworthiness Directives; Airbus Model A330-200 and A330-300 Series Airplanes, and Airbus Model A340-200 and A340-300 Series Airplanes
airworthiness · Rule · Final rule. · Published 2006-07-05 · Effective 2006-08-09 · 71 FR 38062
Document
Document number
06-5943
Federal Register citation
71 FR 38062
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A330-200 and A330-300 Series
Publication date
2006-07-05
Effective date
2006-08-09
FAA docket
Docket No. 2002-NM-247-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A330-200 and A330-300 series airplanes; and Airbus Model A340-200 and A340-300 series airplanes. This AD requires lubrication of the upper and lower shortening mechanism (SM) link of the main landing gear, and consequent detection of resistance or blockage of the greaseway. Depending upon the resistance finding and upon whether or not the airplane has a certain modification, this AD also requires various other actions including unblocking the greaseway; accomplishing all necessary repairs; performing various inspections; and accomplishing the eventual replacement of the SM8 pin, if necessary. This action is necessary to prevent failure of the landing gear lengthening system, which could result in reduced controllability of the airplane on the ground during landing. This action is intended to address the identified unsafe condition.