As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE INSPECTION ACCORDING TO ALLEGIANT WORK CARD: 532180-01-2-001, THE FASTENER HEADS OF THE EXISTING EXTERNAL DOUBLERS WERE FOUND WITH CORROSION AND AFTER REMOVAL WERE FOUND ELONGATED HOLES. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND THE CORRODED AREA WAS REPAIRED FOLLOWING AIRBUS REPAIR INSTRUCTIONS UNDER DOSSIER 81375337 AS PER COOPESA ENGINEERING ORDER COO-EO-2024-19775 REV. 01 AND ALLEGIANT ERO R5321-0042 REV. 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P107 NRI 1-46.