As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON INITIAL INSPECTION IAW SA-167, THE FOLLOWING ABNORMALITIES WERE DISCOVERED. CYLINDER NR 2 INTAKE PUSHROD (ROCKER ARM END) AND ROCKER ARM WERE ABNORMALLY WORN. CYLINDER NR 4 INTAKE PUSHROD (ROCKER ARM END) AND ROCKER ARM WERE ABNORMALLY WORN. THESE PARTS WERE PREVIOUSLY REPLACED AT ENGINE TIME SINCE NEW OF 1090.0 ON 9/14/2016. SEE SDR 2016FA0000436 DATED 09/19/2016 FOR REFERENCE. TOTAL TOME ON THIS ENGINE SINCE NEW: 1103.8 HOURS. TIME SINCE PUSHRODS AND ROCKER ARMS WERE REPLACED AGAIN: 13.8 HOURS.