As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) LARGE HYDRAULIC LEAK FOUND IN TAIL AREA. WIRING HARNESS FOR RUDDER SYNCHRO TRANSIMTTER CHAFED THROUGH RETURN LINE FOR NR 2 RUDDER ACTUATOR. WIRING HARNESS WRAPPED WITH SPIRAL WRAP. LEAK FOUND IN UPPER PORTION OF LINE JUST BELOW RUDDER SYNCHRO TRANSMITTER.