AVIATION ENGINES
AVIATION ENGINES
TOA 288
Two cylinder, horizontal opposed, air cooled, two cycle engine, with fuel saving electronic engine management system and mixture lubrication. Suitable for pusher and tractor installations.

Performance: | 14,5 kW (19,7 HP) at 6’500 rpm On request up to 17 kW (23 HP) at 6500 rpm |
Fuel efficiency | < 380 g/kW/h @ 6’000RPM and 14,0 kW (full load) < 300 g/kW/h @ 4’500RPM and 8,0 kW (cruise) |
Bore: | 56 mm / 2.20 inch |
Stroke: | 58.5 mm / 2.30 inch |
Displacement: | 288 cm³ / 17.58 cu. Inches |
Weight: | 9,3 kg (incl. exhaust, wiring loom, ECU, air intake, Fuel pump with filters and pressure regulator, 1 kW Starter / Generator) |
Crankshaft: | high strength steel, single piece connecting rods with needle bearings |
Throttle control: | integrated SERVO, controlled via ECU |
Cylinders: | Casted aluminum, Nickel-Silicium coated barrel |
Ignition System: | CDI (Capacitor Discharge Ignition), controlled by ECU |
Engine Management system: | 12V Digital integrated fuel and ignition control unit incl. cold start and altitude compensation and EGT and CHT overheat protection |
Altitude compensation: | Automatic via ECU |
Fuel: | Gasoline min. 91 Oct. or AVGAS LL100, mixed with synthetic two-cycle oil to the ratio of 2% |
Optional Equipment: | • Oil injection +0,25kg • 1 kW / +28VDC SGCU (Starter Generator Central Unit) +1,7 kg • 500 W / +28VDC GCU (Generator Central Unit) +0,5 kg • Double ignition +0,35 kg |
Installation: | horizontal, vertical |