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ROTAX ® is the
registered trademark of
Bombardier-Rotax GmbH.
 
 

582 UL - D.C.D.I. Mod. 99

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

 

Version

Performance

Torque

Max rpm

kW

hp

1/min

Nm

ft. lb.

1/min

1/min

582 UL-2V

40

53.6

6000

68

50.1

5500

6400

582 UL-2V

48

65.0

6500

75

55.3

6000

6800

 

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

 

Fuel

Super 2-stroke motoroil

Mixing Ratio

min. MON 83 RON 91
min. AKI 87
leaded or unleaded

API –TC- Classification

1:50
(variable with fresh oil pump)

 

Ignition Unit

Ignition Timing

Spark Plug

DUCATI double CDI

18° v.OT

ROTAX part number 897 055

 

Generator Performance

R.P.M.

Voltage

155 W DC

6000 1/min

13.5 V

   

! 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.

Weight

kg

lb

standard

engine

29.1

64.0

2 carburetor

1.8

4.0

exhaust system

5.1

11.2

options

double air filter

0.5

0.7

electric starter

3.5

7.7

gearbox B / i = 2.0/2.24/2.58

4.5

9.9

gearbox C / i = 2.62/3.0/3.47/4.0

8.0

17.6

gearbox E / i = 2.62/3.0/3.47/4.0

11.2

24.7

external alternator 220 W DC

1.1

2.4

2 radiators big

2.2

4.9

radiator 995 697

1.0

2.2

expansion tank 922 317

0.3

0.7

overflow bottle 922 325

0.2

0.4

fresh oil pump

0.3

0.2

oil tank 2.4 L

1.2

1.3

HAC-kit

0.2

0.4

intake silencer 2V

1.1

2.4

after muffler

1.6

3.5

instrument FLYdat

0.5

1.1

recall instrument RDAT

1.0

2.0

 

Two conical air filters

0.3

0.7

   


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