What was found
ON FINAL APPROACH THE NR 2 ENGINE EXPERIENCED A FLAME OUT CONDITION AND THE PILOT WAS ABLE TO LAND THE AIRCRAFT SAFELY WITH ONLY POWER FROM THE #1 ENGINE. A GENERAL VISUAL INSPECTION OF THE FIRST STAGE COMPRESSOR SECTION REVEALED NO DAMAGE. A GENERAL VISUAL INSPECTION OF THE THIRD STAGE TURBINE WHEEL REVEALED DAMAGE. A BORESCOPE OF THE HOT SECTION ALSO REVEALED DAMAGE. A GENERAL VISUAL INSPECTION OF THE FUEL NOZZLES REVEALED NO DAMAGE OR UNUSUAL WEAR. A GENERAL VISUAL INSPECTION OF THE ENGINE INLET REVEALED NO DAMAGE. DAMAGE TO THE THIRD STAGE TURBINE WHEEL WAS LIKELY CAUSED BY DEBRIS FROM THE HOT SECTION, HOWEVER; NO DEFINITIVE CAUSE FOR THE DAMAGE IDENTIFIED IN THE HOT SECTION WAS DETERMINED.