AD 2018-03-06

final rule
Data completeness: 80%

Airworthiness Directives; Airbus Airplanes

AD Number
2018-03-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2018-0029
FR Citation
83 FR 5301

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-201 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Inappropriate upper beam installation during production can cause an abnormal bending load on the bolt, leading to fracture.

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

Required Actions

Contact the FAA to obtain instructions for addressing the unsafe condition, and do the actions specified in those instructions. The actions include repetitive ultrasonic inspections of the aft mount-pylon bolts of each engine and, depending on findings, corrective actions.

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

Compliance Time

Before further flight

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

Affected Aircraft

Airbus Model A330-201, -202, -203, -301, -302, and -303 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.