What was found
(CAN) #2 HYDRAULIC QUANTITY SYSTEM AT ZERO. #2 HYDRAULIC SYSTEM LINE FROM ENGINE DRIVEN HYDRAULIC PUMP FOUND CHAFED AND LEAKING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) #2 HYDRAULIC QUANTITY SYSTEM AT ZERO. #2 HYDRAULIC SYSTEM LINE FROM ENGINE DRIVEN HYDRAULIC PUMP FOUND CHAFED AND LEAKING.