The CMD19 TC is a four-cylinder four-stroke, horizontally-opposed, turbocharged, liquid-cooled, gasoline engine design, with a mechanical gearbox reduction drive. Gear RR 2.667:1
The engine produces 180 hp (132 kW) for take-off @ 5800 rpm and 177 hp (130 kW) continuous.
The engine in its basic configuration can produce rated power up to 15,000 ft (4,572 mt).
The product development strategy aims to achieve 20,000 ft (6096 mt) with a high altitude turbocharger.
It can be used for ultralight aircrafts, tactical UAV, recreactional and commercial purposes.