As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL ON THE LEFT SIDE. THE FRAME WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2400=5, REV IR, 3-5-01.