Fuselage — Frame 72 Fairing Hardpoints — Inspection
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform a detailed inspection of the fuselage fairing joints at frame 72 before the aircraft exceeds 12,300 flight cycles since manufacture and repeat inspections every 4,100 flight cycles thereafter. If cracks are found, affected parts must be replaced before the next flight. After replacement, the first inspection can be deferred to 12,300 flight cycles following installation, with subsequent inspections following the original intervals.
Summary
EASA Airworthiness Directive 2023-0033 is an airworthiness directive issued by EASA concerning Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the fuselage fairing hardpoints at frame 72 to detect potential fatigue cracks that could compromise structural integrity. The directive applies specifically to affected aircraft identified by manufacturer serial numbers in the referenced Airbus Service Bulletin.
What changed
This new airworthiness directive introduces repetitive detailed inspections of the fuselage fairing joints at frame 72 on both left-hand and right-hand sides. It requires replacement of any cracked parts found during inspections and allows deferral of the first inspection after part replacement to 12,300 flight cycles. No previous directives are superseded by this AD.
Why it matters
This directive is critical for maintaining the structural integrity of Airbus A380 aircraft by addressing potential fatigue cracking in a key fuselage area. Operators and maintenance organizations must comply to prevent possible structural failures that could affect flight safety. Compliance ensures continued airworthiness and regulatory adherence under EASA rules.
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