As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TAKE-OFF FROM THE AIRPORT (PTY), THE FAULT MESSAGE “F/CTL SLAT SYS 2 FAULT” WAS SHOWN IN THE ECAM DISPLAY AND BY FACILITIES OF MAINTENANCE AND PARTS STOCK IT WAS DECIDED TO DIRECT THE AIRCRAFT TO THE MAIN BASE (MDE) AND NOT (LIM) AS IT WAS SCHEDULED. THE SLAT AND FLAP CONTROL COMPUTER WAS REPLACED IN ACCORDANCE WITH THE AIRBUS MAINTENANCE MANUALS AMM 27-51-34-000-801-A, AMM 27-51-34-400-801-A AND AMM 27-54-00-710-802-B. THE TEST WAS SUCCESSFUL. SLAT AND FLAP CONTROL COMPUTER INFORMATION: PN OFF: 84333-00-0305, SN OFF: 84333000003417 PN ON: 84333-00-0305, SN ON: 84333000004721