Customization: | Available |
---|---|
Transport Package: | Box |
Origin: | China |
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Rotax 912 ULS | S Aircraft Engines |
WEIGHT | kg | lb |
Engine with propeller speed reduction gearbox i = 2.43 with overload clutch | 56.6 | 124.5 |
Overload clutch | 1.7 | 3.7 |
Exhaust system | 4.0 | 8.8 |
External alternator | 3.0 | 6.6 |
Engine mount | 2.0 | 4.4 |
Air guide hood | 0.4 | 0.8 |
PERFORMANCE | ||
73.5 kW | 100 | 5800 1/min. |
TORQUE | ||
128 Nm | 94 ft. lb. | 5100 1/min. |
Max RPM |
5800 1/min. |
BORE | |
84.0 mm | 3.13 in |
STROKE | |
61.0 mm | 2.4 in |
DISPLACEMENT | |
1352 cm³ | 82.6 cu in |
FUEL* |
min. MON 85 RON 95* min. AKI 91* |
Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
* leaded, unleaded, AVGAS 100LL, Ethanol 10
** max. continuous power at 5500 1/min