AD 2012-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-243 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the hinges integrated into the 12 o'clock beam of the thrust reversers, which could result in separation of a thrust reverser from the airplane, and consequent reduced controllability of the airplane.
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Required Actions
Remove certain C-duct assemblies of the left- and right-hand thrust reversers from service at specified life limits, as outlined in Table 1 of the AD. The removal must be performed in accordance with a method approved by the FAA or EASA.
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Compliance Time
Within 3 months after the effective date of this AD, or before the accumulation of specified total flight cycles, depending on the C-duct assembly part number.
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Affected Aircraft
All Airbus Model A330-243, -243F, -341, -342, and -343 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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