As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 258.5 TO STRINGER 24P CLIP IS CORRODED. REMOVED STRINGER CLIP IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW 53-30-15-00-01. INSTALLED NEW STRINGER CLIP IAW SRM 51-42-05-02-01. APPLIED CPC IAW AMM 51-25-01-390-801.