AD 2005-19-28
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Model A330-301, -321, -322, -341, and -342 Airplanes; and Model A340-200 and A340-300 Series Airplanes |
Unsafe Condition
Fatigue cracks in the vertical web of the wing rear spar between ribs 1 and 2, propagating from the build slot to the nearest adjacent bolt hole.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the aft face of the rear spar at the area adjacent to the bolt holes and the end of the build slot for cracks using high-frequency eddy current (HFEC) inspections. Repair any cracks found according to specified procedures, including re-profiling the end radius of the build slot to reduce stress concentration. Terminate inspections after re-profiling is completed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight for any crack extending beyond fastener holes 'B' and within a specified modification cut-out area.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A330-301, -321, -322, -341, and -342 airplanes; and Model A340-200 and A340-300 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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