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 533152-01-7-001 ON STRINGER 41 LH AT FR33+230MM SPOT CORROSION WAS FOUND. THE STRINGER WAS REPAIRED FOLLOW THE REPAIR INSTRUCTIONS IAW A320 SRM 53-21-13-300-018 FIG 001. THIS IS A PERMANENT REPAIR CAT B AND MUST BE INSPECTED IAW A320 SRM 53-21-13-205-018 TABLE 1.THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P182 ITEM 1-25.