As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING UPPER SKIN AFT STRINGER END IS CRACKED BETWEEN RIB 19 AND 20. TRIMMED OUT CRACKED PORTION OF STRINGER END IAW SRM 51-10-02-0G. HFEC IAW NDT PART 6; 51-00-00 PROC 23 & 16; 53-30-00 PROC 5. NO DEFECTS NOTED. INSTALLED 3 EA. FASTNERS COMMON TO STRINGER THAT WERE REMOVED FOR ACCESS IAW SRM 51-40-02-0G; AND DRAWING 112A3001 REV-.