As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CLIMBOUT NR 1 BLEED LIGHT ON, NO PRESSURIZATION ACCOMPANIED BY REGULATOR FAULT LIGHT. NR 2 BLEED HIGH TEMP LIGHT ACCOMPANIED BY BLEED FAULT LIGHT. REMOVED AND REPLACED NR 1 ENGINE IAW ENA EO 008-08 AND A300 AMM CHAPTER 71-00-00 PAGES 401 THRU 448. GROUND CHECKS NORMAL, NO LEAKS NOTED. REMOVED AND REPLACED FAN AIR VALVE AND PRECOOLER IAW A300 AMM CHAPTERS 36-11-15 AND 36-11-16. GROUND CHECKS NORMAL DURING ENGINE RUNS.