As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIRED CORRODED AREAS OF THE UPPER INBOARD SKINS OF THE LH & RH WINGS ALONG AND UNDERNEATH THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING ATTACH ANGLES) BY R&R THE DRAG ANGLES, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS FOUND ACCEPTABLE AND FABRICATED AND INSTALLED REPAIR DOUBLER TO LH WING AS REQUIRED PER TEXTRON FIELD REPAIR.