AD 2014-16-25

final rule
Data completeness: 80%

Airworthiness Directives; Airbus Airplanes

AD Number
2014-16-25
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0061
FR Citation
79 FR 52184

Applicability

TypeManufacturerModelDetails
aircraft Airbus A330-200 and A330-300 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Fatigue cracking at the circumferential joint of frame 53.3, which could lead to reduced structural integrity of the fuselage.

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

Required Actions

Reinforce the structure of the center fuselage at the upper circumferential joint of frame 53.3 within new thresholds, as specified by the referenced service information.

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

Compliance Time

Within the new thresholds specified in the referenced service information.

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

Affected Aircraft

Airbus Model A330-200 and A330-300 airplanes, as specified in the referenced service information.

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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