AD 2024-16-15

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus SAS Airplanes

AD Number
2024-16-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2024-0223
FR Citation
89 FR 78226

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS Airworthiness Directives; Airbus SAS Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus SAS Airplanes

Unsafe Condition

Reports of quality non-conformity on main landing gear (MLG) axles where the HVOF coating on the bearing journal runout areas had a coating thicker than allowable limits. This over-thickness could lead to damage, cracking, or spalling of the protective coating, which could expose the base material and allow corrosion to develop, potentially resulting in MLG axle failure and MLG collapse.

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Required Actions

Repetitive inspections of the affected MLG axles for any discrepancy, including damage, cracking, or spalling of the HVOF coating, or corrosion. Corrective actions, including obtaining and following repair instructions, and eventual replacement of affected parts. Prohibition of the installation of affected parts or MLGs having an affected part installed.

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Compliance Time

Before further flight

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Affected Aircraft

Airbus SAS Model A330-200, A330-200 freighter, A330-800, A330-900 series airplanes; Model A330-301, -302, -303, -323, -342, and -343 airplanes; and Model A340-312 and -313 airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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