AD 2016-01-03

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2016-01-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-1981
FR Citation
81 FR 1504

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 Freighter Airworthiness Directives; Airbus Airplanes

Unsafe Condition

The inner bore of some main landing gear (MLG) unit bogie beams were insufficiently re-protected against corrosion after inspection or maintenance actions, leading to potential corrosion and collapse of the MLG unit.

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Required Actions

Determine which revision of the component maintenance manual (CMM) was used for the most recent MLG unit overhaul. Conduct a detailed inspection for missing or damaged paint, and if necessary, inspect the cadmium plating for discrepancies, measure its depth, and inspect the base metal for corrosion or damage. Inspect repaired areas for cracking or corrosion. Take corrective actions if necessary, including removing cadmium plating, repairing damaged areas, re-applying cadmium plating and paint, and re-applying temporary corrosion protection to the bores of the MLG bogie beams.

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

Compliance Time

Within 12 months of the effective date (February 17, 2016)

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Affected Aircraft

Airbus Model A330-200 Freighter, A330-200, A330-300, A340-200, and A340-300 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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