As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE LOWER RIGHT FUSELAGE SKIN JUST UNDER THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 53-00-01 FIGURE 201 SHEET 5 AND EMBRAER FAX NR SST-1515/00 DATED JUNE 12, 2000.