EASA AD 2026-0119-E: Wings – Wing Mid Spars – Inspection

What to do

Operators of affected Airbus A380 aircraft must contact Airbus immediately for inspection instructions and complete the special detailed inspections within the specified compliance times—before the next flight for Group 1 aircraft and within 25 flight cycles for Group 2. Any discrepancies found must be repaired per Airbus instructions before further flight. Inspection results must be reported to Airbus within 7 days after inspection or the effective date.

Summary

EASA Airworthiness Directive 2026-0119-E is an emergency directive addressing inspection requirements for the wing mid spars on Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates special detailed inspections to detect cracks that could compromise wing structural integrity. The directive applies to certain serial numbers grouped into two categories with different compliance times.

What changed

This new emergency airworthiness directive introduces additional special detailed inspections of the wing mid spars on affected Airbus A380 aircraft following findings of cracks in previous inspections. It requires operators to contact Airbus for inspection instructions, perform the inspections within specified flight cycles, and report results. This AD is an interim measure and may be followed by further actions.

Why it matters

This directive is critical for maintaining the structural integrity of the wing on affected Airbus A380 aircraft, directly impacting flight safety. Operators, maintenance organizations, and compliance teams must ensure timely inspections and repairs to prevent potential failures. Non-compliance could result in grounding of aircraft or unsafe flight conditions.

What to do

Summary

What changed

Why it matters

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