[Correction] Wings — Leading Edge Shear Cleats — Inspection / Replacement
- Published
- Effective
- Replaces
- 2015-0141R4
- Replaces
- 2012-0052R1
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 affected shear cleats before exceeding 2,500 flight cycles since first flight and repeat inspections every 2,500 flight cycles or 18,400 flight hours, whichever occurs first. If cracks are found, affected shear cleats must be replaced before the next flight, followed by additional inspections and corrective actions. Installing the applicable Airbus modification service bulletin terminates the repetitive inspection requirement.
Summary
EASA Airworthiness Directive 2015-0141R5 is a regulatory update addressing inspection and replacement requirements for leading edge shear cleats on Airbus A380-841, A380-842, and A380-861 aircraft. The directive mandates detailed inspections and corrective actions to detect and fix cracks found during fatigue testing on specific wing shear cleats. It applies to all serial numbers except those with certain Airbus production modifications.
What changed
This revision 5 of EASA AD 2015-0141 adds reference to the final applicable Airbus modification service bulletin A380-57-8089, which was previously omitted. It also includes editorial standardization changes without altering the core requirements. No further revisions are planned or expected.
Why it matters
This directive is critical for maintaining the structural integrity of Airbus A380 wings by ensuring early detection and repair of cracks in shear cleats. Compliance helps operators avoid potential safety risks and ensures adherence to continuing airworthiness obligations. Maintenance and compliance teams must integrate these inspections and possible modifications into their scheduled maintenance programs.
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