As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORRODED AREAS ON THE UPPER AND LOWER SURFACES OF THE EMERGENCY EXIT DOOR ALONG THE CONTOUR RINGS. BLENDED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS, NO CRACKING INDICATIONS FOUND. PERFORMED ULTRASONIC THICKNESS INSPECTION. REPLACED TWO BLIND RIVETS NEAR THE OUTER HANDLE, CLEANED, ETCHED, ALODINED AND PRIMED BARE METAL AREAS IAW ENGINEERING REPAIR MEMO.