What was found
(CAN) IN-FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. HOSE FOUND CRACKED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) IN-FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. HOSE FOUND CRACKED.