Engine
C20F is a family of two-cylinder, two-stroke, dual-ignition aircraft engines designed for powered paragliders, one and two place powered parachutes, single place ultraliht trikes, light single place ultralight aircraft and motor gliders.
2-cylinder
2-stroke air-cooled engine with opposed cylinders
With reduction drive
Diaphragm carburetor
Dual electronic ignition
Electric starter
With exhaust mufflers
Engine mount assembly
SFC at cruise: 485 g/kW.h
TBO 300 h
WEIGHT | KG | |
Engine with propeller speed reduction drive | 18.5 | |
Exhaust system | 2.8 | |
PERFORMANCE | ||
20 kW | 27 hp | 6800 RPM |
MAX RPM | 6800 RPM | |
BORE | STROKE | |
66 mm | 55 mm | |
DISPLACEMENT | FUEL | |
342 cm³ | Min. 92 Mogas or Avgas |
single paramotor
Fix-wing aircraft
Delta wing
double paramotor