Aviation engines2020-03-23T10:10:45+00:00

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

Power Curve

Power curve of TOA288

BSFC Curve

BSFC curve of TOA288
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