What was found
EXAMINATION TO DETERMINE CAUSE OF ENGINE FAILURE DISCLOSED NR 1 CYLINDER HAD CRACKED APPROXIMATELY THREE-FOURTHS OF THE BARREL CIRCUMFERENCE CAUSING LOSS OF OIL QUANTITY AND PRESSURE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXAMINATION TO DETERMINE CAUSE OF ENGINE FAILURE DISCLOSED NR 1 CYLINDER HAD CRACKED APPROXIMATELY THREE-FOURTHS OF THE BARREL CIRCUMFERENCE CAUSING LOSS OF OIL QUANTITY AND PRESSURE.