AD 2015-23-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the upper shell structure of the fuselage between Frame (FR) 80 and FR86, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the upper shell structure of the fuselage between FR80 and FR86 using high frequency eddy current (HFEC) inspections. Repair any cracking found. Modify the upper shell structure as necessary to improve fatigue tolerance.
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Compliance Time
Within specified intervals, as defined in the referenced service bulletins and AD requirements.
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Affected Aircraft
Airbus Model A330-200, A330-300, and A340-300 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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