Engine 916i 160 HP
Engine 916i 160 HP
160 hp (119 kW) at 5800 rpm for takeoff, 137 hp (102 kW) at 5500 rpm continuous
General characteristics
- Type: Four-cylinder, four-stroke aircraft engine
- Bore: 84.0 mm (3.3 in)
- Stroke: 61.0 mm (2.4 in)
- Displacement: 1,352 cc (82.5 cu in)
- Dry weight: 85.8 kg (189.2 lb), including propeller speed reduction gearbox with overload clutch, turbocharger, intercooler, and exhaust system.
- Components
- Turbocharger: inter-cooled.
- Fuel system: electronic fuel injection
- Fuel type: gasoline minimum MON 85, RON 95, AKI 91, leaded or unleaded, avgas 100LL, maximum ethanol 10%
- Oil system: dry sump, forced lubrication with separate oil tank
- Cooling system: air-cooled with liquid-cooled cylinder heads
- Reduction gear: mechanical gearbox, 2.54:1 ratio