What was found
DURING INITIAL CLIMB, THE ECAM MASTER CAUITON F/CTL R AIL FAULT, 5 MINUTES LATER, F/CTL AIL SERVO FAULT. IAW AMM 27-14-51, PB 401. THE AILERON SERVO CONTROL WAS REPLACED .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INITIAL CLIMB, THE ECAM MASTER CAUITON F/CTL R AIL FAULT, 5 MINUTES LATER, F/CTL AIL SERVO FAULT. IAW AMM 27-14-51, PB 401. THE AILERON SERVO CONTROL WAS REPLACED .