As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF PAINT, THE TECHNICIAN FOUND CORROSION ON RT OTBD WING LOWER SURFACE AT MULTIPLE LOCATIONS, BETWEEN RIBS 13 - 23. THE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF CRACK DEFECTS. MINIMUM THICKNESS REMAINING AFTER CORROSION REMOVAL IS .074 INCHES. IAW EO ATR-57-2014.