As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE NR 2 ENGINE FLAMED OUT WHILE ON FINAL APPROACH. ALL APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT BLEED VALVE CONTROLLER TO BE AT FAULT. THE CONTROLLER WAS REMOVED AND REPLACED IAW MM 75-32-0. IN ADDITION, THE HP FUEL PUMP AND FUEL FLOW GOVERNOR WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD DURING ENGINE RUN.