As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CREW REPORTED HYDRAULIC SYSTEM NR 2 ZERO PERCENT QUANTITY AND ZERO PRESSURE. RAMP REPORTED A LARGE QUANTITY OF FLUID UNDER AFT FUSELAGE. MAINTENANCE FOUND THE NR 2 HYDRAULIC SHUTOFF VALVE LEAKING DUE TO THE VALVE BODY SPLIT. MAINTENANCE REMOVED AND REPLACED THE SHUTOFF VALVE IAW CRJ MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)