As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION AS PER ALLEGIANT WORK CARD 554003-01-1-001 AND REMOVAL OF RUDDER TO COMPLY WITH NON ROUTINE ITEM 3-52 WAS FOUND RH UPPER AND LOWER HOIST POINTS LOOSE AND DAMAGED. PERFORMED PERMANENT REPAIR CAT A AT RUDDER SHELL SKIN PANEL RH AROUND UPPER # 3 HOIST POINT IAW A320 SRM 55-41-13-300-029 PARAG 2A AND AROUND LOWER FWD # 2 HOIST POINT IAW A320 SRM 55-41-13-300-030 PARAG 2A