As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IN COMPLIANCE WITH AD 2006-25-02, X-RAY RESULTS INDICATED SEVERE CORROSION IN AFT FUSELAGE AREA RT OF FUSELAGE, AFT OF PRESSURE BULKHEAD, BETWEEN TAIL ACCESS DOOR AND APU DOOR. CORROSION IS LOCATED BETWEEN STR 11 AND 13. ALL REPAIRS MADE IAW ENGINEERING REPORT.