As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE COCKPIT LH WINDOW FRAME LATERAL POST DAMAGED/ELONGATED RETAINER ATTACHMENT HOLES SHANK AND TOOL MARK. CORRECTIVE ACTION DAMAGED HOLES SHANK (QTY3) AND UPPER SURFACE TOOL MARK BLENDED-OUT AND INSPECTED, PERFORMED DVI, PLUS DYE PENETRANT PLUS EDDY CURRENT INSPECTION AT EACH HOLE TO CONFIRM ABSENCE OF SCRATCH, CRACK OR ANY OTHER DISCREPANCY, FOLLOWING ATR INSTRUCTION REF. ES_00224792_01 ISSUE A.