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 TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR68 RH DOR STOP FITTING # 1 HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME AT FR68RH STOP FITTING #1 IAW A320 SRM TASK 53-41-12-300-011 PARAG 2A FIG 008 AND COOPESA EO# COO-EO-2025-21724-R00. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q008 ITEM 2-55.