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/CREW DOOR CUT OUT AT FR68 LEVEL STGR 8L FRAME VERTICAL INTERNAL RADIUS CRACK WAS FOUND. AIRBUS WAS CONTATCED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDE REPAIR INSTRUCTIONS AND FR 68 STGR 8L WAS REPAIRED FOLLOW REPAIR REPAIR INSTRUCTIONS AS PER COOPESA EO COO-EO-2024-19382-R01 AND ALLEGIANT ERO R5341-0118-R00. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P009 ITEM 2-61.