As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INFLIGHT, NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED AND ASSOCIATED LOSS OF NR 2 HYD QTY, NR 2 SYSTEM .7 REMAINS. FOUND NR 2 SYSTEM PRESSURE LINE LEAKING IN FLAP WELL BETWEEN FUSELAGE AND NR 1 NACELLE. REMOVED RIDGED LINE AND INSTALLED TEMP FLEX LINE IAW SPEC PROCEDURE 20.1. LEAKED CHECKED GOOD AT THIS TIME.