Oaxaca Aerospace began the project in 2011 with the objective of designing an agile, fast and inexpensive two-seat airplane and concluded in mid-2013, the year in which the ground tests began. The aircraft has a rear mounted
Lycoming AEIO-390 engine, canards and a tandem design cockpit with dual flight controls. The rear seat is at a higher level with respect to the front seat, which allows a view of 300° vertical and 240° horizontal. The aircraft was first presented to the public at Feria Aeroespacial México (FAMEX) 2015. == Specifications ==