912 A2

912 A2 is a piston engine model used in aircraft.

Specifications

Engine Family: piston

Bore: 79.5 millimetre

Compression ratio: 9

Cooling system: Liquid & air

Cylinder configuration: Horizontally opposed

Cylinder count: 4

Displacement: 1211 cubic-centimetre

Dry weight: 57 kilogram

Fuel grade: RON 90

Fuel type: Mogas

Height: 0.38 metre

Length: 0.59 metre

Max. continuous RPM: 5500

Max. continuous hp: 78 horsepower

Max. takeoff RPM: 5800

Max. takeoff hp: 80 horsepower

Stroke: 61 millimetre

Width: 0.58 metre

Control system: Dual channel FADEC