What was found
ON CLIMB, LOSS OF NR 1 HYDRAULIC FLUID QUANTITY. C/A - FOUND PRESSURE LINE FROM NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE PUMP AND HYDRAULIC LINE. SERVICED SYSTEM, BLED SYSTEM, OPERATIONAL CHECK NORMAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON CLIMB, LOSS OF NR 1 HYDRAULIC FLUID QUANTITY. C/A - FOUND PRESSURE LINE FROM NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE PUMP AND HYDRAULIC LINE. SERVICED SYSTEM, BLED SYSTEM, OPERATIONAL CHECK NORMAL.