What was found
ENGINE REMOVED DUE TO #1 AND #2 WHEEL CYCLE RETIREMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 1ST STAGE WHEEL BLADES MINOR SULFIDATION AND ERODED LEADING EDGE. SCRAPPED 1ST STAGE WHEEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE REMOVED DUE TO #1 AND #2 WHEEL CYCLE RETIREMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 1ST STAGE WHEEL BLADES MINOR SULFIDATION AND ERODED LEADING EDGE. SCRAPPED 1ST STAGE WHEEL.