Summary
We are superseding Airworthiness Directive (AD) 2007-06-12 for certain Airbus Model A330-200 and A330-300 airplanes. This new AD reduces the compliance times for reinforcing the structure of the center fuselage. This AD was prompted by a new fatigue and damage tolerance evaluation that revealed the compliance time for an existing reinforcement of the fuselage has to be reduced. We are issuing this AD to prevent fatigue cracking of the fuselage, which could result in reduced structural integrity of the fuselage.
Directive Details
AD Number
FAA-2014-0061
Document Number
2014-19725
Type
Rule
Publication Date
September 3, 2014
Effective Date
October 8, 2014
Affected Manufacturer
Airbus
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2014-0061
Topics
Official Documents
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