Abstract: Universiti Kuala Lumpur Malaysian Institute of Aviation Technology (UniKL MIAT) had acquired a static flight simulator of type Boeing 737 NG. Before the arrival of the simulator, a Factory Acceptance Test (FAT) was actuated in order to confirm the simulator would arrive according to the specifications and also within the correct conditions. FAT was also actuated to gauge the functionality of the components of the simulator and to confirm that it would be delivered according to the timeline. This paper delineated the FAT procedures that was implemented and the corresponding results of the FAT.