As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ENGINE WAS INDUCTED IN THE SHOP FOR HIGH PRESSURE NOZZLE GUIDE VANE (NGV) BURNS. ON DISASSEMBLY OF ENGINE, TWO VANES WERE FOUND TO HAVE THE COMPLETE LEADING EDGE BURNED AWAY. THE METAL LOSS EXTENDED TO THE MIDSPAN INTERNAL BULKHEAD OF THE VANE. THE PARTS WERE REMOVED FROM SERVICE. PART TC: 9,411.