As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE REMOVED DUE TO LOW POWER AND OIL LEAKING. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 50% OF 1ST STAGE WHEEL SULFIDATED AND DELAMINATED ON FORWARD SIDE OF BLADES AND EROSION OF ALL LEADING EDGES AND BLADE TIPS. SCRAPPED 1ST STAGE WHEEL.