Searchable Light Aviation Database

Atec 212 Solo

Performance & specifications:

Stall speed: 40 mph (64 kph)
Cruise speed: 137 mph (220 kph)
Never exceeded speed: 180 mph (290 kph)
Empty weight: 441 lbs (200 kg)
Gross weight: 661 lbs (300 kg)
Atec 212 Solo

212 Solo`s description

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.

Manufactured / designed by the same producer / designer:

Atec 321 Faeta

EW: 606 lbs (275 kg)
MTOW: 1041 lbs (472 kg)
Vs0: 32 mph (51 kph)
Vc: 141 mph (227 kph)
Atec 321 Faeta

Atec Zephyr 122

EW: 584 lbs (265 kg)
MTOW: 1213 lbs (550 kg)
Vs0: 40 mph (64 kph)
Vc: 134 mph (216 kph)
Atec Zephyr 122

Comparable airplanes:

Morgan Aeroworks Super Diamond MkII

EW: 408 lbs (185 kg)
MTOW: 992 lbs (450 kg)
Vs0: 43 mph (68 kph)
Vc: 138 mph (222 kph)
Morgan Aeroworks Super Diamond MkII

ULM Speedmax Racer

EW: 419 lbs (190 kg)
MTOW: 694 lbs (315 kg)
Vs0: 40 mph (64 kph)
Vc: 143 mph (230 kph)
ULM Speedmax Racer