As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE S/N CD0019 HAD A BURNT HOLE EXPOSING INNER CAVITY AT LEADING EDGE OF ONE BLADE. BORESCOPES ON OTHER ENGINES IN FLEET HAVE REVEALED SINGLE CRACKS AT CENTER OF VARIOUS BLADE TIPS; 2 CRACKS (NON-CONVERGING) AT CENTER OF BLADE TIP; MINOR COATING LOSS AT LEADING EDGE OF ALL TURBINE BLADES. DAMAGE NOTED IS WITHIN LIMITS PER DORNIER 328J JIC TR 72-087. ENGINE S/N`S CD0019 AND CD0022 WERE REMOVED TO BE SENT TO REPAIR FACILITY.