As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - MAJOR - DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CREASED FORWARD OF FR 9 AND BELOW STR 15R. AFTER INITIAL REWORK THE AREA WAS STILL CREASED, HAD MINOR OIL CANNING AND MINOR WAVINESS OUT OF SRM LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EC5330-01635 AND EMB 145 SRM 53-10-01, TYPE A REPAIR, SECTION2, FIG 201 SHEET 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.