What was found
AFTER LANDING, DURING FLAPS RETRACTION, THE SLAT DRIVE NON NORMAL CONDITION OCCURRED. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURE IAW AMM DMC-B787-A-27-81-00-00B-320A-A, TESTED CORRECT. ADDITIONALLY FLIGHT CONTROL MODULE WAS REPLACED IAW DMC-B787-A-27-02-18-00A-720A-A, TESTED CORRECT.