As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING ROUTINE INSPECTION A FUEL LEAK WAS NOTED ON THE NR 2 CYLINDER AROUND THE INTAKE PORT. UPON FURTHER INVESTIGATION, A CRACK WAS NOTED IN THE CYLINDER WALL JUST ABOVE THE INTAKE PORT. THE CRACK IS APPROXIMATELY 1" IN LENGTH. THE CYLINDER WAS REPLACED AND THE ACFT RETURNED TO SERVICE.