What was found
(CAN) #2 HYDRAULIC QUANTITY AT ZERO. DRAG STRUT ACTUATOR LINE FOUND CHAFED AND LEAKING. LINE REPLACED
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) #2 HYDRAULIC QUANTITY AT ZERO. DRAG STRUT ACTUATOR LINE FOUND CHAFED AND LEAKING. LINE REPLACED