As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE INSPECTION PROCESS AS PER ALLEGIANT ENGINEERING ORDER E5316-0003 REV. 01RELATED TO SB 53-1330 REV. 00, IT WAS FOUND THE FWD FUSELAGE - FR16 - DOOR STOP FITTING LOCATION #7 WITH CRACK INDICATION. THE DETAILS WERE SENT TO AIRBUS ASKING FOR REPLACEMENT INSTRUCTIONS AND FINAL APPROVAL.THIS REPAIR IS COVERED WITH COOPESA JOB A1N200 ITEM 2-36