As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK FUSELAGE FLOOR SKIN CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 61-62 STRINGERS 21L-21R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN FRAMES 61-62 STRINGERS 21L-21R IAW EMB-145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.