AD Amdt-39-11347
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Model A330-301, and Model A340- 211, -212, -311, and -312 Series Airplanes |
| aircraft | Bell | Various | Airworthiness Directives; Airbus Model A330-301, and Model A340- 211, -212, -311, and -312 Series Airplanes |
Unsafe Condition
Fatigue cracking of the fuselage belly fairing support structure, which could result in reduced structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive detailed visual inspections of the fuselage belly fairing support structure to detect cracks. Take corrective action if cracks are found. Optional terminating action is provided for the repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A330-301 and Model A340-211, -212, -311, and -312 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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