This paper outlines an approach for creating a more efficiently flying vehicle by using a figure -8 flapping motion. The process spanning from design concept to prototyping testing is discussed. A simple mechanical transmission system was developed in order to create a flap with two degrees of freedom. The figure 8 flapping motion is compared with other designs that create a similar motion. The primary purpose of this design is to serve as the first step towards a flapping wing MAV with fully controllably wing path dictation. The device has been test in the load cell with some degree of success showing the ability to generate a net force up to 50% its own weight (3.8g).