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Aquila A210

	Engine
Bombardier Rotax 912 S	4 cylinder
T/O power	73,5 kW / 100 HP
Maximum continous rating	69 kW / 95 HP
MTV-21-A/175-05	2-Blade Constant Speed propeller

	Dimension
Length	7.3 m
Height	2.3 m
Span	10.3 m
Wing area	10.5 m²

	Mass
DOW	190 KG
MTOW	750 KG
max. payload	260 KG
max. cargo	40 KG
Fuel capacity	2 x 60 litre (100LL/Eurosuper)

	Flight performance parameters
Maximum speed	165 kt
Cruising speed	130 kt (MSL)
Stall speed	50 kt (V s1)
Stall speed	43 kt (V so)
Service ceiling	14.500 ft
Best rate of climb	3,8 m/s (MSL)

	T/O- and landing distances
T/O roll	250 m
T/O distance	470 m (with 15m obstacle clearance)
Landing roll distance	200 m
Landing distance	500 m (with 15m obstacle clearance)