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54hp or 65hp, 2 cylinder, 2-stroke water cooled engine with dual electronic ignition. Comes complete with twin carbs, exhaust system, rewind starter and fuel pump.
£POA | |
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Version |
Performance |
Torque |
Max rpm |
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kW |
hp |
1/min |
Nm |
ft. lb. |
1/min |
1/min |
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582 UL-2V |
40 |
53.6 |
6000 |
68 |
50.1 |
5500 |
6400 |
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582 UL-2V |
48 |
65.0 |
6500 |
75 |
55.3 |
6000 |
6800 | |
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Bore |
Stroke |
Displacement |
Compression ratio |
|
76 mm |
2.99 in |
64 mm |
2.52 in |
580.7 cm3 |
35.44 cu.in |
th:11.5 |
ef: 5.75 |
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Fuel |
Super 2-stroke motoroil |
Mixing Ratio |
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min. MON 83 RON 91 min. AKI 87 leaded or unleaded |
API –TC- Classification |
1:50 (variable with fresh oil pump) | |
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Ignition Unit |
Ignition Timing |
Spark Plug |
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DUCATI double CDI |
18° v.OT |
ROTAX part number 897 055 | |
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Generator Performance |
R.P.M. |
Voltage |
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155 W DC |
6000 1/min |
13.5 V | |
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! Warning !
This aircraft engine does not comply with federal safety regulations for standard aircraft. This engine is for use in experimental and ultralight uncertified aircraft only and only in circumstances in which an engine failure will not compromise safety. Before operating the engine read operators manual. Information is available from your local authorised ROTAX distributor. | |
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Weight |
kg |
lb |
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standard |
engine |
29.1 |
64.0 |
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2 carburetor |
1.8 |
4.0 |
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exhaust system |
5.1 |
11.2 |
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options |
double air filter |
0.5 |
0.7 |
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electric starter |
3.5 |
7.7 |
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gearbox B / i = 2.0/2.24/2.58 |
4.5 |
9.9 |
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gearbox C / i = 2.62/3.0/3.47/4.0 |
8.0 |
17.6 |
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gearbox E / i = 2.62/3.0/3.47/4.0 |
11.2 |
24.7 |
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external alternator 220 W DC |
1.1 |
2.4 |
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2 radiators big |
2.2 |
4.9 |
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radiator 995 697 |
1.0 |
2.2 |
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expansion tank 922 317 |
0.3 |
0.7 |
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overflow bottle 922 325 |
0.2 |
0.4 |
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fresh oil pump |
0.3 |
0.2 |
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oil tank 2.4 L |
1.2 |
1.3 |
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HAC-kit |
0.2 |
0.4 |
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intake silencer 2V |
1.1 |
2.4 |
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after muffler |
1.6 |
3.5 |
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instrument FLYdat |
0.5 |
1.1 |
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recall instrument RDAT |
1.0 |
2.0 |
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Two conical air filters |
0.3 |
0.7 | |
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