Airframe Dimensions
Wing Span	10.8 m
Airframe Length	6.1 m
Total Height	2.1 m
Wing Area	11.4 m2
Aspect Ratio	9.5
Wing Chord-max	1.2 m
Wing Chord-min	0.655 m
Airfoil Section	SM 701
Performance Details Rotax 912 80hp Engine
Max Speed VNE	118 kts
Cruise Speed	90 kts
Stall Speed	35 kts
Rate of Climb	900 fpm
Max Range	700 nm with Long Range Tanks
Take off run	150 m
Take off to clear 15m	250 m
Landing run	100 m
Landing over 15m obstacle	220 m
Other Data
Undercarriage	Tricycle
Main Wheel Track	1.55 m
Suspension	Sprung composite undercarriage legs
Wheel brakes	Hydraulic brakes
Tyre Dimensions
Main wheels	14 x 4 (350 x 100)
Nose wheel	14 x 4 (350 x 100)
Engines
Rotax 912	80 hp
Rotax 912S	100 hp
Fuel tank volume (Standard)	63 litre /47 kg fuel
Standard fuselage tank	63 litre
Extra Wing tanks (optional)	2 x 20 litre
Weights
Maximum Take-off Weight	520 kg (600 kg currently being certified)
Empty Weight	280 kg
Maximum useful load	240 kg
Minimum Front-Seat Pilot Weight	55 kg
Baggage Weight	10 kg
Operation Limitations
Wing flaps	Lever position	Flaps Deflection	Never Exceed Speed
Cruise position	0	-4.5 degrees	VNE 118 Knots
Take-off	1	+15 degrees	VFE 60 Knots
Landing	2	+48 degrees	VFE 60 Knots
Stall speeds at MTOW 520 kgs - level flight
Wing Flaps Position	Engine Power Output	IAS Knots	CAS Knots
0	Engine at idle	46 Knots	43 Knots
1	Engine at idle	40 knots	39 knots
2	Engine at idle	37 knots	35 knots