212 Solo

by Atec
3.8
8
212 Solo - Photo #1

A single-seater, cantilever low-winged all composite aircraft. High volume of carbon together with honeycomb sandwich reinforcements provide a very low weight and high strength and rigidity. It’s design is derived from well-proven types ZEPHYR 2000 and especially ATEC 321 FAETA from which the shortened wing of SM 701 profile with high-efficient slotted flaps is used.

Source:www.atecaircraft.eu

Specifications

Empty weight:
441 lbs (200 kg)
MTOW:
661 lbs (300 kg)
Stall speed:
35 kts (40 mph) (65 kph)
Cruise speed:
130 kts (150 mph) (241 kph)
VNE:
157 kts (181 mph) (291 kph)
Climb:
1000 ft/min (5.1 m/s)
Engine:
Rotax 582

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