As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE CLEATS AND STRINGERS CRACKED AND CORRODED IN THE FOLLOWING AREAS, CLEAT AT LOWER LONGERON LT SIDE CRACKED AT FRAME ATTACHMENT FS 216.125 2 LT SIDE STRINGER CORRODED ON END AT FS 190.6 3. CLEAT AT STRINGER 6 LT HAS RIVETS MISSING AT FS 227.