What wing component showed cracks during routine maintenance on affected A380s?

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Cracks were found in a structural beam running along the A380 wing during routine maintenance

Cracks were reported in a key wing component described as a structural beam that runs along the wing and carries much of the aerodynamic load during flight. The issue was identified during routine maintenance checks, after inspections were ordered by the European Union Aviation Safety Agency (EASA) following earlier findings of cracks in the wing-spar structure.
The cracked part was a structural beam along the wing
The affected component is a structural beam that extends along the wing. It is described as carrying much of the aerodynamic load during flight, which is why it was singled out in the inspection directive.
The cracks were detected during routine maintenance checks
Inspectors found the cracks while carrying out routine maintenance checks on the affected Airbus A380 aircraft. The inspections were triggered by those findings and then formalised through EASA-ordered urgent examinations.
The inspections focused on the wing-spar structure area
The inspections were ordered after cracks were found in the wing-spar structure. The wing-spar is part of the wing’s structural system, and the cracked beam component is presented as part of that load-bearing arrangement.
The directive followed cracks found in EASA-ordered checks
EASA issued an urgent directive in December 2025 that required airlines to examine the wing-spar structure after cracks were discovered. Airbus then moved to inspect 16 A380 planes, with five scheduled for immediate inspection after the cracks were identified in the described wing component.

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What wing component showed cracks during routine maintenance on affected A380s?

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