AD 2012-25-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-200 and -300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Premature fracture of the main landing gear (MLG) bogie beam due to high tensile standing stress from dry fit axle assembly method, which could result in the airplane departing the runway, the bogie beam detaching, or MLG collapse, leading to structural damage and injury.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace all affected MLG bogie beams with new or serviceable parts before reaching the new reduced life limits or within 6 months after the AD's effective date, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6 months after the effective date of the AD or before reaching the new reduced life limits, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A330-200 and -300 series airplanes, all manufacturer serial numbers, with specific part numbers 201485300, 201485301, 201272302, 201272304, 201272306, or 201272307, except those with S/N S2A, S2B, or S2C.
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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