What was found
(CAN) DURING FINAL, NR 2 HYDRAULIC PRESSURE WAS AT 2700 PSI, 10 SECONDS LATER PRESSURE AT ZERO. NR 2 HYDRAULIC SWITCH SELECTED TO OFF. CONTROLS CHECKED FOR BINDING. AFTER SHUTDOWN, LEAK FOUND IN NOSE WHEEL AREA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING FINAL, NR 2 HYDRAULIC PRESSURE WAS AT 2700 PSI, 10 SECONDS LATER PRESSURE AT ZERO. NR 2 HYDRAULIC SWITCH SELECTED TO OFF. CONTROLS CHECKED FOR BINDING. AFTER SHUTDOWN, LEAK FOUND IN NOSE WHEEL AREA.