What was found
RIGHT HYD SYSTEM LEAK AT PYLON. REMOVED NR 2 ENGINE THRUST REVERSER ISOLATION VALVE HYD PRESSURE LINE. REPLACED LINE WITH A FLEXIBLE LINE IAW GPM 1-0-13-003 PG 10. OPS AND LEAK CHECKED OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT HYD SYSTEM LEAK AT PYLON. REMOVED NR 2 ENGINE THRUST REVERSER ISOLATION VALVE HYD PRESSURE LINE. REPLACED LINE WITH A FLEXIBLE LINE IAW GPM 1-0-13-003 PG 10. OPS AND LEAK CHECKED OK.