What was found
(AUS) HYDRAULIC PRESSURE HOSE LOCATED BETWEEN THE RH ENGINE DRIVEN HYDRAULIC PUMP AND THE FIREWALL HAD FAILED. LOSS OF HYDRAULIC FLUID.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) HYDRAULIC PRESSURE HOSE LOCATED BETWEEN THE RH ENGINE DRIVEN HYDRAULIC PUMP AND THE FIREWALL HAD FAILED. LOSS OF HYDRAULIC FLUID.