As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER T/O ECAM INDICATED SLATS SYS 2 FAULT AND OVER-HEAD INDICATED SLATS SYS 2 FAULT LIGHT ILLUMINATED. CREW CYCLED SLATS TWICE - SLATS AND FLAPS WERE NORMAL AFTER SECOND CYCLE - LIGHT REMAINED ILLUMINATED. NR 2 SFCC FAULTED HIGH SPEED VALVE. REPLACED SLAT SYS 2 VALVE BLOCK ASSY 26CV IAW MM 27-84-33-04, OPS CHECK 27-84-00. RAN SLATS THROUGH SEVERAL TIME NO FAULTS ON OVERHEAD NR 2 SYS.