EASA AD 2026-0030 — Wings — Movable Flap Track Fairings 2 and 5 / Forward Attachments — Inspection
Summary
EASA Airworthiness Directive 2026-0030 is issued for Airbus A380-841, A380-842, and A380-861 aeroplanes concerning the movable flap track fairings 2 and 5 forward attachments. It mandates inspections to detect potential structural issues caused by unexpected aerodynamic loads on these parts. The directive applies to all serial numbers except those with specific Airbus modifications or service bulletins already incorporated.
What Changed
This new airworthiness directive introduces repetitive inspections of the forward attachments of movable wing flap track fairings 2 and 5 to identify any structural damage. It also provides an optional terminating modification that reinforces the affected parts, eliminating the need for further repetitive inspections once applied. The directive includes detailed instructions on inspection intervals and corrective actions based on findings.
Why It Matters
This directive is critical for maintaining the structural integrity of the Airbus A380 wing trailing edge components, preventing possible detachment of flap track fairings that could damage flight control surfaces. Compliance ensures continued airworthiness and safety, reducing the risk of in-flight structural failure and potential injury on the ground. Operators and maintenance teams must integrate these inspections and modifications into their maintenance programs to meet regulatory requirements.
What To Do
Operators must inspect the affected flap track fairing forward attachments within 8,200 flight cycles from first flight and repeat inspections every 400 flight cycles thereafter, following Airbus Service Bulletin A380-57-8280. If discrepancies are found, corrective actions must be taken as specified. Alternatively, applying the reinforcing modification per Airbus Service Bulletin A380-57-8141 Revision 01 will terminate the inspection requirements. Compliance with these actions is mandatory starting from 12 March 2026.