As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLENDED MULTIPLE CORRODED AREAS OF THE RH WING UPPER INBOARD SKINS LOCATED ALONG THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE), PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDED AREAS BY TREATING, PRIMING AND TOP COATING AREAS PER TEXTRON STANDARD REPAIR.