As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) TAKEOFF WAS ABORTED DUE TO ENGINE VIBRATION, WHICH WAS HEAVIEST AT 92% N2, AND UNSTABLE ENGINE PARAMETERS. ICING CONDITIONS WERE PRESENT. NEITHER CLEANING NOR FUEL BLEED CLEARED THE PROBLEM. VISUAL INSPECTION FOUND THE LOW PRESSURE TURBINE DAMAGED, WITH A BLADE MISSING.