As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 534135-01-4-001 , UPPER FUSELAGE AFT PAX DOOR CUT OUT AT FR68 STGR 8RH FRAME VERTICAL INTERNAL RADIUS CRACK WAS FOUND. AIRBUS WAS CONTATCED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED SRM REFERENCE TO PERFORM THE REPAIR. THE FR 68 STGR 8R WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS AS PER A320 SRM 53-41-12-300-012. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P009 ITEM 2-60.