|
Rotax® 914UL DCDI |
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4 cylinder, 4 stroke liquid/air cooled engine with opposed cylinders, with turbo charger, automatic waste gate control, dry sump forced lubrication with seperate 3l (.8 gal US) oil tank, automatic adjustment by hydraulic valve tappet, 2 CD carburetors, electronic dual ignition, electric starter, integrated reduction gear i= 2.243, engine truss assembly, air intake system, exhaust system. |
|
Version |
Performance |
Torque |
Max RPM | ||||
|
|
kW |
HP |
RPM |
Nm |
ft. lb. |
RPM |
RPM |
|
914 UL2 |
73.5 |
100 |
5500 |
144 |
106 |
4900 |
5800 |
|
Max 5 min (take-off) |
84.5 |
115 |
5800 |
|
|
|
|
|
Bore |
Stroke |
Displacement |
Compression
| ||||
|
79.5 mm |
3.13 in. |
61 mm |
2.4 in. |
1211.2 cm3 |
73.91 cu. in. |
9.0:1 | |
|
Options | |
|
914 UL3 |
Suitable for
'Constatnt Speed' propellers. |
|
914 UL4 |
Suitable for 'fixed pitch'
propellers |
|
|
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GmbH.