AD 2017-14-01

Recurring final rule
Data completeness: 90%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-14-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-3984
FR Citation
82 FR 31245

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Corrosion and cracking of the bogie beams under the bogie stop pad, which could result in bogie beam detachment, main landing gear collapse, or runway excursion.

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

Required Actions

Conduct repetitive detailed inspections for damage and corrosion of the sliding piston sub-assembly. Perform investigative actions including corrosion and damage tests on the bogie assembly base material and magnetic particle inspections for cracks, corrosion, and damage of the bogie beam. Repair affected parts. Replace main landing gear (MLG) with improved bogie beams as a terminating action for repetitive inspections.

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

Compliance Time

Within specified compliance times revised in this AD.

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Affected Aircraft

Airbus Model A330-200, -200 Freighter, and -300 series airplanes; and Model A340-200 and -300 series airplanes. Excludes Model A340-500 and -600 series 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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