TECHNICAL DATA AND PERFORMANCE

Max take off weight

600 kg (1,323 lbs.)

Empty weight

290 kg (640 lbs.)

Fuel quantity

2 x 50 L (27 US Gallons)

Max fuel load

76 kg (168 lbs.)

Max payload (including fuel)

310 kg (684 lbs.)

Load factors (at weight 540 kg)

+6 –3 G

Load factors (at weight 600 kg)

+5.4 –2.7 G

 

 

Wing span

10,830 mm (35 ft 7 in.)

Wing mean chord

958 mm (37.7 in.)

Flaperon chord

25%

Wing area

10.6 Sq. M (115 Sq. ft.)

Wing aspect ratio

11.3

Wing airfoil

NACA 64 - 418 (modified)

Wing dihedral

Zero deg.

Wing weight (approx.)

66 kg (145 lbs.)

Wing wetted area (approx.)

23 sq. M (250 sq. ft.)

Span loading

52.63 kg/m (35.25 lbs/ft)

 

 

Fuselage length

6,720 mm (22 ft 1 in.)

Fuselage max width

760 mm (30 in.)

Fuselage height (fuselage horizontal)

2,150 mm (85 in.)

Fuselage weight (approx.)

230 kg (507 lbs.)

Fuselage wetted area (approx.)

15 sq. M (160 sq. ft.)

Vertical fin area (approx.)

1.8 sq. M (20 sq. ft.)

Vertical fin airfoil

NACA 64-010

Vertical fin tail arm (approx.)

3.4 M (7.5 ft.)

 

 

Horizontal Stabilizer span

2.6 M (28 sq. Ft.)

Horizontal Stabilizer chord

550 mm (22 inch.)

Horizontal Stabilizer area

1.4 sq. M (15 sq. ft.)

Horizontal Stabilizer aspect ratio

4.8

Horizontal Stabilizer airfoil

NACA 64-012

Horizontal Stabilizer tail arm

3.62 M (11.9 ft.)

Horizontal Stabilizer weight (approx.)

8 kg (18 lbs.)

Horizontal Stabilizer wetted area (approx.)

2.9 sq. M (31 sq. ft.)

 

 

POWER PLANT

 

Make and model

Jabiru 2200(Rotax 912 ULS)

 

 

PERFORMANCE

 

Max horizontal speed (540 kg) gnd. level

190 km/hr (102 kt.)

Cruise speed 75% power

170 km/hr (92 kt.)

Most economical speed 40% power

148 km/hr (80 kt.)

Stall speed (540 kg) clean

80 km/hr (43 kt.)

Stall speed (540 kg) flaps and gear

70 km/hr (38 kt.)

Max climb rate (540 kg)

5 m/s (990 ft/min.)

Max maneuver speed (540 kg)

213 km/hr (115 kt.)

Speed never exceed (approx.)

282 km/hr (152 kt.)

 

 

Endurance cruise speed 65%

7.6 hours without reserve

Range at cruise speed 65%

1,200 km (650 nautical miles)

Mileage

8 liter/100 km (29 mpg)

 

 

Endurance most economical speed

12 hours without reserve.

Range at most economical speed

1,700 km (918 nautical miles)

Mileage

6 liter/100 km (39 mpg)