AD 2008-14-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 and A340-300 | Airworthiness Directives; Airbus Model A330-200 and A340-300 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A330-200 and A340-300 Series Airplanes |
Unsafe Condition
Loss of integrity of the upper shell structure of the fuselage between frames (FR) 84 and FR87.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the upper side shell structure between frames 84 and 87 using a high frequency eddy current (HFEC) method. Repair any cracks found. Contact Airbus for further instructions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A330-200 and A340-300 series airplanes, all serial numbers on which Airbus Modification 44205 has been embodied in production, except those with Modifications 52974 or 53223.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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