As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS - ENG 1 BLEED FAULT AFTER ENG START. REMOVED AND REPLACED CLEVIS AND SCREW PIN OF ELECTROPNEUMATIC ACTUATOR ON ENG1 PERFORMED OPS TEST OF BMC 1 TEST PASSED. PERFORMED ENG RUN OF ENG 1 NO ECAM MESSAGES ENG RUN GOOD OK TO CONTINUE PER AMM 36-11-504-400-802A.