What was found
DURING C-CHECK THE FUSELAGE EXTERNALLY HAS 2 GOUGES BETWEEN FR 2 AND 3 STR 17 R. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB 145XR SRM 53-11-01 FIG 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK THE FUSELAGE EXTERNALLY HAS 2 GOUGES BETWEEN FR 2 AND 3 STR 17 R. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB 145XR SRM 53-11-01 FIG 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.