airworthiness · Rule · Final rule. · Published 2015-11-24 · Effective 2015-12-29 · 80 FR 73092
Document
Document number
2015-28886
Federal Register citation
80 FR 73092
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2015-11-24
Effective date
2015-12-29
FAA docket
Docket No. FAA-2015-0490
Abstract
We are superseding Airworthiness Directive (AD) 2008-22-20 for certain Airbus Model A330-200, A330-300, and A340-300 series airplanes. AD 2008-22-20 required repetitive high frequency eddy current (HFEC) inspections for cracking, repair if necessary, and modification of the upper shell structure of the fuselage. This new AD shortens certain compliance times. This AD was prompted by a determination from a fatigue and damage tolerance evaluation that the compliance times must be reduced. We are issuing this AD to prevent fatigue cracking of the upper shell structure of the fuselage, which could result in reduced structural integrity of the airplane.