ATEC 212 Solo for Sale
Discover new & pre-owned ATEC 212 Solo aircraft for sale worldwide on AvPay. The ATEC 212 Solo, a Czech-built ultralight aircraft celebrated for its lightweight composite construction and efficient performance, is popular among sport and recreational pilots. Find ATEC 212 Solo airplanes for sale in the USA, North America, UK, Europe, Asia, Africa, Australia, and South America. Buy ATEC 212 Solo planes directly from aircraft brokers, private sellers, flying clubs, flying schools, and manufacturers. Explore our complete aircraft for sale inventory Here.
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Interesting facts about the ATEC 212 Solo
✈ The ATEC 212 Solo is a single seat ultralight from the Czech Republic, produced by ATEC in Libice nad Cidlinou.
✈ The airframe uses a high volume of carbon composite with honeycomb reinforcement for low weight and high strength.
✈ The wing spans 7.48 m and uses the SM701 airfoil with slotted flaps for low stall speeds and short field performance.
✈ Engine options include the 65 hp Rotax 582 two stroke and the 80 hp Rotax 912 UL four stroke.
✈ Prototype flights began in 2005, and the model was designed to meet FAI microlight rules.
✈ Standard fuel is a 50 L fuselage tank, with an optional wing tank set of 2 x 35 L for touring range.
✈ Operational limits classify it for day VFR only. Aerobatics, intentional spins, and IFR are not permitted.
✈ Pilot weight limits in the manual specify a minimum of 65 kg and a maximum of 90 kg for correct balance.
ATEC 212 Solo Specifications
Information provided here is as a guide only. Do not use this information for flight planning or aircraft operations. Model variations, modifications, upgrades, and age affect the figures shown. Always check precise specifications with the seller, the manufacturer, or your aviation authority.
Length: 5.20 m (17 ft 1 in)
Wingspan: 7.48 m (24 ft 6 in)
Height: 1.55 m (5 ft 1 in)
Empty Weight: 200 kg (441 lb) minimum, Rotax 582, central tank
Max Take Off Weight (MTOW): 300 kg (661 lb)
Fuel Capacity: 50 L standard fuselage tank; optional wing tanks 2 × 35 L (total 70 L)
Cruise Speed: 200 km/h (124 mph, 108 kt) at 4,270 rpm, approx. 12.2 L/h
Range: 1,036 km (643 mi, 560 nm) at 140 km/h IAS with 30 min reserve
Service Ceiling: Not published
Rate of Climb: 8.5 m/s (1,700 ft/min) at 120 km/h IAS
Take-off Run to 15 m (49 ft): 190 m (620 ft) concrete; 215 m (700 ft) turf
Landing Distance: 120 m (394 ft)
FAQs About the ATEC 212 Solo
How much does an ATEC 212 Solo cost?
Pricing varies with engine, avionics, and options. In 2024 to 2025, new factory builds commonly ranged from about $95,000 to $110,000. Well kept used examples in 2024 to 2025 often listed below new build pricing depending on hours and equipment.
What engines are available on the ATEC 212 Solo?
Buyers typically choose between the 65 hp Rotax 582 two stroke and the 80 hp Rotax 912 UL four stroke. Many buyers prefer the 912 UL for lower fuel burn per knot and stronger climb performance.
What runway length does the ATEC 212 Solo need?
The take off distance to 15 m is 190 m on concrete and 215 m on turf. The landing distance is about 120 m. Actual figures depend on density altitude, weight, surface, and technique.
How far can the ATEC 212 Solo fly on standard tanks?
At 140 km/h IAS, the flight manual shows about 1,036 km with a 30 minute reserve on the standard tank setup. The optional wing tanks increase endurance for touring.
Is the ATEC 212 Solo suitable for training?
It is a single seat aircraft. Instructors use it for post license proficiency and sport flying rather than dual instruction. Training usually occurs in two seat types, then pilots step into the Solo for personal flying.
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