As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIRED THE LH UPPER WING SKIN LOCATED UNDER AND ADJACENT TO THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE) BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON FIELD REPAIR BY CLEANING, TREATING, AND PRIMING AREAS.