As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT CRASHED AFTER TAKEOFF. POST-CRASH INSPECTION REVEALED NR 4 CYLINDER EXHAUST PUSHROD BROKEN AT VALVE END. NR 4 EXHAUST VALVE NOT IN OPERATION DUE TO BREAK OF PUSHROD. AD 80-25-02 AND AD 95-03-10 WERE ISSUED PERTAINING O-235 PUSHRODS. TWO OTHER PUSHROD INCIDENTS WERE NOTED FROM CESSNA OWNER'S ORGANIZATION MAGAZINE, MARCH '96 ISSUE. SUBJECT PUSHROD IAW OF AD 80-25-02 AND AD 95-03-10.