What was found
DURING APPROACH AND SLAT EXTENSION, RECEIVED ECAM. SLAT SYS 1 FAULT. & FLAPS SYS 1 & 2 FAULT. CYCLE PER ECAM. FAULT DID NOT CLEAR. ALL 3 FAULTS RETURNED INCLUDING AMBER ECAM KRUGER NOT EXTENDED. COMPLIED WITH QRH DECLARED EMERGENCY & LANDED. LT FLAPS SLATS EXTENDED FOR INSPECTION AFTER LANDING. NO FAULTS NOTED DURING POST FLIGHT INSPECTION, PERFORMED BITE PROCEDTURE ON SFCC 1 AND 2 IAW TSM 27-50-00, NO FAULTS FOUND, PERFORMED FLAPS & SLATS OPS TEST MULTIPLE TIMES IAW AMM 27-54-00-05, OPS TEST GOOD, INSPECTED SLATS / KRUEGER FLAPS IAW AMM 27-80-00-00, NO DAMAGE NOTED. A/C OK FOR SERVICE.