What was found
(AUS) LT ENGINE FIRST STAGE TURBINE BLADE FAILED. EXTENSIVE SECONDARY DAMAGE TO HOT SECTION COMPONENTS. SOME DAMAGE TO COMPRESSOR SECTION DUE TO IMBALANCE OF THE ROTATING COMPONENTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) LT ENGINE FIRST STAGE TURBINE BLADE FAILED. EXTENSIVE SECONDARY DAMAGE TO HOT SECTION COMPONENTS. SOME DAMAGE TO COMPRESSOR SECTION DUE TO IMBALANCE OF THE ROTATING COMPONENTS.