AD 2001-15-29
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Model A330-301, -321, -322, -341, and -342 Series Airplanes and Airbus Model A340 Series Airplanes |
Unsafe Condition
Fatigue cracking of the bottom skin and reinforcing plate of the wing due to bending, which could lead to reduced structural integrity of the airplane wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforcement of the wing structure at the inboard pylon rear pickup area must be performed. This is to be accomplished by following the applicable Airbus Service Bulletins.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
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 series airplanes, and Airbus Model A340 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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