As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION CHECK FOUND CORROSION ON FUSELAGE SKIN BETWEEN STA 340 TO 360, LONGERON 32 RT TO 32 LT. CORRODED AREA WAS REMOVED AND EXTERNAL DOUBLER, FILLER DOOR JAMB INNER SKIN AND SPLICE WERE FABRICATED AND INSTALLED IAW EWO ATI 53-042. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.