AD 2018-25-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Cracking at fastener holes located at a certain frame on the lower shell panel junction, which could lead to reduced structural integrity of the fuselage.
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Required Actions
Repetitive special detailed inspections (rototest) of certain fastener holes located at the lower shell junction of a certain frame on both left-hand (LH) and right-hand (RH) sides, and applicable related investigative and corrective actions, including oversizing, installing fasteners and repair, and accomplishment of applicable related investigative actions, which include a rototest inspection for cracking after oversizing.
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Compliance Time
Within 50 flight hours
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Affected Aircraft
All Airbus SAS Model A330-223F and Model A330-243F airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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