As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FUSELAGE FRAME 42 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3674-3, REV IR, 6-12-00.