As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE HAS AN OIL LEAK AT 6 O'CLOCK AFT PART OF REVERSER COWL. AFTER VISUAL INSPECTION FOUND HYDRAULIC LEAK FROM LINES UNDER HEAT SHIELD BLANKET FOR EDP. REPLACED PRESSURE HOSE FROM J-BOX TO HYD PUMP. CLEANED AREA LEAK CHECKED GOOD.