As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C M/D BS1140 LBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1" BY 3" EXCEED SRM LIMIT. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 ORIGINAL THICKNESS .0445" BLEND OUT DEPTH 0.028" BY 1" BY 3" WITHIN SRM 57-30-01 FIG 1 LIMITS. INSPECTION WITH 10X MAGNIFING GLASS.