As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION ON STRINGER CLIP AT STA 6.7 STRINGER 25P. REMOVED CORROSION IAW SRM 51-21-00. CLIP FOUND TO BE OUT OF LIMITS IAW SRM 53-20-23. REMOVED STRINGER CLIP IAW SRM 51-42-05. FABRICATED NEW STRINGER, ALODINED AND PRIMED IAW DWG 853295. INSTALLED NEW STRINGER CLIP IAW SRM 51-42-05. COMPLIED WITH TASK CARD 6-53-1059.