As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) CONNECTING ROD END CAP SEPARATED - PRELIMINARY INVESTIGATION INDICATES FAILURE IN AREA APPROXIMATELY 10MM (0.393IN) ABOVE THE BOLT SHOULDER ON THE CAMSHAFT SIDE BEHIND THE HARD FACE FOR THE BEARING SHELL PROGRESSING OUTWARDS UNTIL FAILURE FROM OVERLOAD -CRANKCASE HOLED IN AREA OF NO1 CYLINDER PUSHROD TUBE FITMENT