As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A SCHEDULED INSPECTION OF THE HYDRAULIC UNIT A CRACK WAS FOUND IN THE SYSTEM 1 VALVE BODY MANIFOLD. THE CRACK ORIGINATES FROM A BLANKING PLUG AND PROGRESSES OUTWARDS APPROXIMATELY 11 MM. NO LEAK OF HYDRAULIC FLUID APPARENT. THIS UNIT WAS RECEIVED FOR INSPECTION FROM A US CUSTOMER. UNIT TOTAL TIME IS 8935.5 HOURS. MANIFOLD TIME NOT KNOWN.