Rotax 912ULS

Top Speed (TAS at sea level) at sea level)

95 kts

Cruise Speed (TAS)

75% power at 5,000 ft.

85 kts

Stall Speed (at max. gross)

No flaps (Vs)

28 kts.

Full flaps (Vso)

26 kts.

Rate of Climb

Solo

1200 f.p.m.

Max. gross

900 f.p.m.

Range (at 75% power)*** (100  litres fuel)

Range Standard Fuel excl. VFR Reserve nm

410 nm

Fuel Consumption (at 75% power) Rotax912

+/- 4 18 l/ph

Service Ceiling (estimated)

14500 ft.

Take off Distance (Clear 50’ obstacle)

Solo

150 m

MTOW

200 m

Landing Distance (Clear 50’ obstacle)

Solo

150 m

MTOW

200 m

Rotax 912 engine (rigged for flight)

6.5 m

Wing Span

Rigged for flight

8.9m

Other Wing Data

Area

12.1 sq. m

Aspect ratio

Wing loading (at max. gross)

49.58 kg/sqm

Structural limit loads (at max. gross)

+ 5 /3 - Gs

Maximum Height

Tricycle

6.5 m

Cabin Dimensions

Width (at hips)

110 cm

Width (at shoulders)

104 cm

Door width

N/A

Door height

N/A

Baggage space / Rear passenger area

0.5 cu/m

Rear door width

N/A

Rear door height

N/A

Weights

Maximum gross weight(on wheels)

544 kg

Maximum gross weight (on floats)

641 kg

Empty weight

320 kg

Useful load

182 kg

Full-fuel payload (standard tanks)

71.9 Kg

Full fuel payload (optional)

N/A

Maximum baggage capacity

35 kg

Fuel Capacity (usable)

Standard tanks

100 ltrs

Option 1

N/A

Option 2

N/A