What was found
NR 1 ENGINE BLEED AIR FAULT, RETURNED TO FIELD. ONLY ABNORMAL WAS BLEED TEMP 300C. ECAM PROC FOLLOWED. CHANGED FAN AIR VALVE THERMOSTAT 644-0035 PER AMM 36-11-43.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE BLEED AIR FAULT, RETURNED TO FIELD. ONLY ABNORMAL WAS BLEED TEMP 300C. ECAM PROC FOLLOWED. CHANGED FAN AIR VALVE THERMOSTAT 644-0035 PER AMM 36-11-43.