As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED SEVERAL LOCATIONS OF DAMAGE TO AREAS WITHIN A BAND APPROXIMATELY 1.0 INCH WIDER THAN WINDOW 8F OPENING INTERIOR SURFACE OF FUSELAGE SKIN. REMOVED BAND OF DAMAGED SKIN 1.0 INCH WIDE FROM AROUND WINDOW OPENING FABRICATED AND INSTALLED INSERTION REPAIR AND EXTERNAL DOUBLER REPAIR.