As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING REAR SPAR AT WBL 95 HAS CORROSION ON WING SKIN. REMOVED CORROSION FROM WING SKIN IAW SRM 57-20-01. PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDT MANUAL 51-00-19. NO DEFECTS NOTED. PERFORMED THICKNESS CHECK OF BLENDED AREA IAW NDT MANUAL 51-00-10, PART 4. DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS AS DEFINED BY SRM. REPAIRED IAW DWG NR 57-13154-1.