Fuselage — Frame 80 Fairing Outboard End Fitting Assemblies — Inspection
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform the initial high-frequency eddy-current inspection before the affected aircraft exceed 14,900 flight cycles since manufacture and repeat inspections every 2,200 flight cycles thereafter. If cracks are found, the fitting assemblies must be replaced before the next flight. After replacement, the first inspection on the new part can be deferred to 14,900 flight cycles post-installation.
Summary
EASA Airworthiness Directive 2023-0034 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the fuselage belly fairing outboard end fitting assemblies at frame 80 to detect potential cracks that could compromise structural integrity. The directive references Airbus Service Bulletin A380-53-8212 for inspection procedures.
What changed
This new airworthiness directive introduces mandatory repetitive high-frequency eddy-current inspections of the fuselage fairing outboard end fitting assemblies at frame 80 on both left-hand and right-hand sides. It requires replacement of any cracked fitting assemblies before further flight and allows deferral of the first inspection after replacement to 14,900 flight cycles. No previous directives are superseded by this AD.
Why it matters
This directive is critical for maintaining the structural integrity of affected Airbus A380 aircraft by preventing crack initiation in key fuselage components. Operators and maintenance organizations must comply to avoid potential safety risks and regulatory non-compliance. Timely inspections and corrective actions help ensure continued airworthiness and operational safety.
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