As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BENDED CORRODED ARE AROUND THE LH WING MIDDLE SPAR AFT SIDE AROUND THE BRAKE LINE BULKHEAD FITTING, PERFORMED ULTRASONIC THICKNESS INSPECTION AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA, APPLIED PRIMER AND TOPCOAT IAW TEXTRON REPAIR DEFINITION.