As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ACTUATOR WAS LEAKING AND REMOVED FROM ACFT, PRESSURE TESTED BEFORE DISASSEMBLY TO CONFIRM LEAK, LEAK FOUND WEEPING THROUGH SIDE OF CYLINDER. SUSPECT AREA CHECKED BY NDT AND CONFIRMED. THIS IS THE SECOND INSTANCE OF THESE CYLINDERS FOUND CRACKED.