AD 2007-08-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 | Airworthiness Directives; Airbus Model A330-200, A330-300, A340-200, and A340-300 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A330-200, A330-300, A340-200, and A340-300 Series Airplanes |
Unsafe Condition
Fatigue damage with a crack propagation through the fastener line of the wing shroud box bottom panel, resulting in panel detachment and potential injuries to persons on the ground.
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Required Actions
Perform a one-time detailed inspection of the shroud box bottom panel for cracks, fasteners missing or loose, damage, and marks; and apply all applicable corrective actions. Do applicable corrective actions before further flight.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes, all certified models, all serial numbers, certificated in any category, on which Airbus Modification 42061 or 46077 or 53604 has been embodied in production and delivered before December 31, 2005.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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