As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A THROUGH FLIGHT TRANSIT CHECK A FLUID LEAK WAS DISCOVERED UNDER THE NR 2 ENGINE. FURTHER INVESTIGATION FOUND AN ADEL CLAMP CHAFFED THROUGH A SOLID HYDRAULIC PRESSURE LINE APPROXIMATELY 12 INCHES FROM THE LOWER END OF THE SOLID LINE. THE SOLID LINE AND ALL SECURING CLAMPS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.