As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED AT THE RH FWD OVERWING EXIT DOOR, ON THE INNER SIDE, IN THE 'CUB STRAP' FROM APPROX. THE CENTER OF THE HATCH OPENING AND FWD. THE CORROSION WAS BLENDED IN ACCORDANCE WITH BACO TELEX DAL-ATL-96-1418RR DATED 11 SEP 96.