AD 2014-16-25
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 and A330-300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking at the circumferential joint of frame 53.3, which could lead to reduced structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforce the structure of the center fuselage at the upper circumferential joint of frame 53.3 within new thresholds, as specified by the referenced service information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the new thresholds specified in the referenced service information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A330-200 and A330-300 airplanes, as specified in the referenced service information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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