AD 2011-14-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-342 | Airworthiness Directives; Airbus Model A330-342 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A330-342 Airplanes |
Unsafe Condition
Fatigue cracking of the internal structure of the fuselage, which could adversely affect the structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive special detailed inspections (ultrasonic inspection) for fatigue cracking of the internal structure of the fuselage corresponding to ALI task 533105-01-02. Repair any cracks in accordance with a method approved by the FAA or EASA (or its delegated agent).
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Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
Airbus Model A330-342 airplanes, manufacturer serial numbers (MSN) 0012 and 0017, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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