Specifications G-200
| Engine Type
|
Naturally aspirated rotary
|
|
|
|
| Displacement
|
3x654cc (3x39.9 cu.in.) per rotor
|
|
| Cooling
|
Coolant: water / ethylene glycol
Coolant heat load: 58kW / 198kBTU/hr
Oil heat load: 26kW / 90kBTU/hr
|
|
| Engine Management
|
Fully redundant dual-ECU digital control
|
|
| Fuel System
|
Dual electronic injection
Dual electric fuel pumps
|
|
| Recommended Fuel
|
100LL avgas
Unleaded mogas (US: 87, Europe: 92)
|
|
| PSRU
|
6-pinion planetary, ratio 2.8235:1
Hydraulic CS propeller governor drive
|
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| Propeller Rotation
|
Tractor configuration: clockwise
Pusher configuration: anti-clockwise
|
|
| Max. Take-off power
|
200 hp @ 2,250 propeller rpm
|
|
| Max. Continuous Power
|
As above
|
|
| 75% Cruise Power
|
150 hp @ 2,050 propeller rpm
|
|
| Weight¹
|
132 kgs / 291 lbs
|
|
| Dual alternators
|
14V 70 Amp or 28V 40A
|
|
¹ Dry engine, PSRU weight including starter, main alternator included
Fact sheet :
