As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLENDED 2 AREAS OF CORROSION ON THE EXTERIOR OF THE FUSELAGE SKIN LOCATED JUST AFT OF THE EMERGENCY EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOP COATED REPAIR AREAS IAW TEXTRON REPAIR MEMO.