What was found
FLIGHT CONTROL LT AILERON FAULT, RT AILERON FAULT, AND ATN LAW ECAMS APPEARED AFTER ROTATION, ELAC 1 FAULT ECAM APPEARED AFTER NR 1 ENGINE SHUTDOWN, THEN DISAPPEARED. IAW TSM 27-93-00-810-949-A, R & R THE NR 1 ELAC IAW AMM 27-93-34. OPS CHECKED GOOD. R & R THE NR 2 ELAC IAW AMM 27-93-34. OPS CHECKED GOOD. PERFORMED LC3CT TEST IAW AMM 22-97-00, TESTED OK