As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND DENTS, SCRATCHES AND CORROSION ON HEAD OF RIVETS AT FUS SKIN BETWEEN STA 720 TO 820, BETWEEN STRINGERS 26 TO 28 LT. STRAIGHTENED AND SMOOTHED PANEL, REMOVED LEVEL ONE CORROSION IAW SRM 51-10-01. CORROSION WITHIN LIMITS OF SRM 53-10-01.