What was found
ENGINE REMOVED DUE TO HIGH T.O.T. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #2 NOZZLE FWD INNER BAND, AFT INNER BAND WELDMENT SEPARATING AND CRACK VANES. INSTALLED A NEW #2 NOZZLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE REMOVED DUE TO HIGH T.O.T. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #2 NOZZLE FWD INNER BAND, AFT INNER BAND WELDMENT SEPARATING AND CRACK VANES. INSTALLED A NEW #2 NOZZLE.