Specifications

ROTAX 582

ROTAX 912

ROTAX 912S

  Empty Weight

248 kg

272 kg 

274 kg 

  Gross Weight

560 kg

560 kg

560 kg

  Useful Load

312 kg

288 kg

286 kg

  Load Factors

+6g  -4g

+6g  -4g

+6g  -4g

  Wing span

9600 mm

9600 mm

9600 mm

  Wing Area

13.25 m²

13.25 m²

13.25 m²

  Chord

1380 mm

1380 mm

1380 mm

  Aspect Ratio

7.01

7.01

7.01  

  Aircraft Length

5670 mm

5670 mm

5670 mm

  Aircraft Height (at Wing)

1900 mm

1900 mm

1900 mm

  Cockpit Height

1370 mm

1370 mm

1370 mm

  Cockpit Width

1200 mm

1200 mm

1200 mm

  Headroom

~850 mm

~850 mm

~850 mm

  Legroom

~1100 mm

~1100 mm

~1100 mm

  Seats

2

2

2

  Luggage Compartment

2 x 25L
(max 35kg)

2 x 25L
(max 35kg)

2 x 25L
(max 35kg)

  Fuel Capacity

100L / 26gal

100L / 26gal

100L / 26gal

  Doors (optional)

2 *

2 *

2 *

Power Plant

  Engine

582 /99 UL

912 UL

912 ULS

  Output

65 HP

80 HP

100 HP

  Gearbox reduction

3.47 : 1

2.27 : 1

2.27 : 1

  Propeller

2/3* Blade

2/3* Blade

2/3* Blade

  Fuel Consumption (at 80%)

~14.5 l/hr

~12 l/hr

~13 l/hr

Performance at sea level at MAUW with doors on

  Take Off roll

100 m

100 m

80 m

  Landing Ground Roll

120 m

100 m

100 m

  Rate of Climb

700 ft/min

730 ft/min

900 ft/min

  Service Ceiling

12000 ft asl

12000 ft asl

14000 ft asl

  Max crosswind component

32 mph

32 mph

32 mph

  Cruise Speed (at 65%)

75 mph

90 mph

100 mph

  Maximum level Speed

100 mp/h

105 mph

110 mph

  Max Speed (VNE)

125 mph

125 mph

125 mph

  Glide Ratio

~10 : 1

~10 : 1 

~10 : 1 

  Power Off Stall (with No flaps)

40 mph

40 mph

40 mph

  Power Off Stall (with flaps)

35 mph

35 mph

35 mph

  Roll Rate

~3 sec 45/45

~3 sec 45/45

~3 sec 45/45

  Endurance (with reserve)

~6.5 hrs

~7.5 hrs

~7.0 hrs

  Range (with reserve)

~500 miles

~670 miles

~700 miles

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