As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) LT ENGINE SECOND STAGE COMPRESSOR BLADE SEPARATED FROM WHEEL. INSPECTION FOUND A SMALL STAIN AT THE BLADE STUMP INDICATING THAT A SMALL CRACK HAD BEEN PRESENT FOR SOME TIME. THE CRACKING HAD BEEN INITIATED BY CORROSION PITTING. THE ADJACENT BLADE HAD A SIMILAR CRACK PRESENT. DAMAGE TO COMPRESSOR AND TURBINE. AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENT BUT HAS REGULAR COMPRESSOR WASHES.