As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, SKIN BULGING AND SCREW PULLING THROUGH LEADING EDGE UPPER AS FRONT SPAR XFS710. REPAIRED IAW DC8 SRM 57-2-1 FIGURE 38. CORROSION TASK CARD NUMBER 107R-0551. NON-ROUTINE TASK CARD NUMBER 81621.