What was found
(CAN) LOST OF HYDRAULIC PRESSURE SYSTEM NR 1 AND QUANTITY IN CRUISE AT FLIGHT LEVEL 310. NO QUANTITY OR PRESSURE FOR 36 MINUTES BEFORE ENGINE SHUTDOWN AFTER LANDING. THE EDP AND THE LEAKING HYDRAULIC PRESSURE LINE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) LOST OF HYDRAULIC PRESSURE SYSTEM NR 1 AND QUANTITY IN CRUISE AT FLIGHT LEVEL 310. NO QUANTITY OR PRESSURE FOR 36 MINUTES BEFORE ENGINE SHUTDOWN AFTER LANDING. THE EDP AND THE LEAKING HYDRAULIC PRESSURE LINE REPLACED.