Atec 212 Solo

Built by the company that builds the Zephyr 2000 and Faeta, this single seat aircraft made in carbon composites first flew in early 2005.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
 useful load
gross weight
fuel capacity
range		 65hp Rotax 582 engine
x
 x
 x
 x
 x
1
 200 kg | 441 lbs
x
 300 kg | 661 lbs
 x
 400 miles

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
 service ceiling		 x
 1000 ft/min | 5 m/s
146 kt
 130 kt 149 mph 240 kmh
x
x

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed 		x
 157 kt 180 mph 290 kmh
35Kts
x

All specifications are based on manufacturer's calculations