The Comp Air Jet will now be powered by an AI-25 TL twin shaft turbofan engine. 3 stages of low pressure driven by a 2 stage turbine, and 9 stages of high pressure driven by a single stage turbine. This engine should have no problems meeting STAGE III noise requirements here in the United States. Fuel control is hydro mechanical with an emergency backup circuit. Bypass ratio is 2.0. Maximum static thrust is 3,780 lbs, typical fuel consumption is 150gph at 25,000 ft at 300 knots.