As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF CLIMB DUAL ENGINE BLEED FAULT APPEARED ON ECAM. AIRCRAFT RETURNED TO BASE NO EMERGENCY WAS DECLARED. NR 1 ENGINE FAN AIR THERMOSTAT WAS REPLACED IAW MM 36-11-43, ALSO NR 2 ENGINE THERMOSTAT FILTER WAS REPLACED. HIGH POWER ENGINE RUN WAS PERFORMED IAW MM 72-00-00, ALL CHECKED OK.