As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ROUTINE HOT SECTION INSPECTION (HSI) FOUND THE ENGINE HAD SUFFERED A FRACTURE OF ONE LP PRESSURE TURBINE BLADE. THE FRACTURE OCCURRED AT 60 PERCENT OF THE BLADE HEIGHT AND CAUSED SECONDARY DAMAGE TO THE BALANCE OF THE LP BLADES AND TO THE OTHER TURBINE COMPONENTS.