What was found
NR 2 CYLINDER CRACK APPROXIMATELY 300 DEGREE CIRCUMFERENCE ON 3RD FIN AREA BELOW SPARK PLUG HOLE. AIRCRAFT HAD A SLIGHT CYLINDER HEAD INCREASE WHICH ALERTED THE PILOT TO SEEK MAINTENANCE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 CYLINDER CRACK APPROXIMATELY 300 DEGREE CIRCUMFERENCE ON 3RD FIN AREA BELOW SPARK PLUG HOLE. AIRCRAFT HAD A SLIGHT CYLINDER HEAD INCREASE WHICH ALERTED THE PILOT TO SEEK MAINTENANCE.