As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THIS LINE ASSEMBLY WAS CHAFING AGAINST AN ENGINE POWER CONTROL CABLE LOCATED BEHIND THE REMOVEABLE LEFT HAND INBOARD LEADING EDGE PANEL. VIBRATION CAUSED THE OUTER SHEATH OF THE CONTROL CABLE TO CHAFE DEEP SERRATIONS INTO THIS LANDING GEAR HYDRAULIC LINE. IT IS RECOMMENDED THE LEADING EDGE BE COMPLETELY REMOVED AT INSPECTIONS TO FACILITATE A MORE THROUGH INSPECTION OF THIS AREA.