As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY BLENDED THREE CORRODED AREAS OF THE EXTERIOR FUSELAGE SKIN, JUST BELOW THE EMERGENCY EXIT OPENING, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED RESULTS TO TEXTRON FOR REPAIR DISPOSITION. TREATED, PRIMED AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.