What was found
LEFT HYDRAULIC QUANTITY DROPPED TO 0.48 UNITS. CREW TURNED OFF BOTH ELECTRICAL HYDRAULIC PUMP AND EDP. *S/D* LEAKING FLEX LINE FROM STAB TRIM MOTOR TO LEFT HYDRAULIC SYSTEM RIGID LINE, AT 'B' NUT COUPLING. FLEX LINE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HYDRAULIC QUANTITY DROPPED TO 0.48 UNITS. CREW TURNED OFF BOTH ELECTRICAL HYDRAULIC PUMP AND EDP. *S/D* LEAKING FLEX LINE FROM STAB TRIM MOTOR TO LEFT HYDRAULIC SYSTEM RIGID LINE, AT 'B' NUT COUPLING. FLEX LINE REPLACED.