As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE ACCOMPLISHMENT OF WORK ORDER 53-260-004 UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT AT FR 68 STRINGER 22 LH WEB HORIZONTAL LOWER FLANGE RADII CRACKED WAS FOUND.AIRBUS WAS CONTACTED ASKING REPAIRINSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68 WAS REPAIRED AS PER COOPESA ENGINEERING ORDER COO-EO-2024-19382-R01 .AND ALLEGIANT ERO R5341-0118-R00.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P009 NRI 2-49.