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-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 DOOR STOP FITTING # 4 UPPER OUTBOARD HOLE WITH CRACK. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FR66 RH DOOR STOP FITTING # 4 IAW A320 SRM TASK 53-41-12-300-008 PARAG 2A(1) FIG 001,002 AND 003 BOX 2 AND 3 AND TASK 53-41-12-300-009 PARAG 2A FIG 001. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q008 ITEM 2-59.