Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
airworthiness · Rule · Final rule. · Published 2005-02-14 · Effective 2005-03-21 · 70 FR 7384
Document
Document number
05-2581
Federal Register citation
70 FR 7384
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300 B2 and B4 Series
Publication date
2005-02-14
Effective date
2005-03-21
FAA docket
Docket No. 2003-NM-16-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD) that applies to all Airbus Model A300 B2 and B4 series airplanes. The existing AD currently requires determining the part and amendment number of the variable lever arm (VLA) of the rudder control system to verify the parts were installed using the correct standard, and corrective actions if necessary. For certain VLAs, this new AD requires repetitive inspections of the VLA and corrective action if necessary. This new AD also provides a terminating action for the repetitive inspections. Furthermore, this new AD reduces the applicability of affected airplanes. The actions specified by this AD are intended to prevent failure of both spring boxes of certain VLAs due to corrosion damage, which could result in loss of rudder control and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.