As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AFTER ENGINE SHUT DOWN AT THE GATE, HYDRAULIC FLUID WAS NOTED LEAKING FROM THE NOSE GEAR AREA. NOSE GEAR DRAG STRUT ACTUATOR HOSE REPLACED DUE TO LEAKING P/N DSC252B40124. DAMAGE FOUND TO BRAIDING JUST AFT OF THE COLLAR DEFECT NR 416542. GEAR RETRACTION CHECKS COMPLETED AND NO LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE.