As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING 100 HR - ROUTINE INSPECTION, RT FWD FUSELAGE SIDE PANEL OPENED UP TO ACCESS TUBING INSPECTION, BOTTOM CABLE FOUND DAMAGED BEHIND SIDE PANEL DOOR TO CABLE CHAFING ON TAIL END OF PANEL SCREW. HOLE BURNED THROUGH CABLE INSTALLATION AND INTO CORE.