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ATEC 212 Solo
ATEC 212 SOLO
ATEC 212 Solo is a single-seater, cantilever low-wing aircraft of carbon composite construction. High volume of carbon together with honeycomb sandwich reinforcement provide a very low weight, but high structural strength. It’s aerodinamically pure design is derived from the design of well-proven ZEPHYR 2000 and ATEC 321 FAETA, especially the wings with SM 701 profile are shortened version of Faeta´s wings fitted with highly efficient slotted flaps. This exceptional airplane has no certification, therefore we offer it only in Experimental KIT version.
Spacious monocoque fuselage is made of carbon composite, reinforced with carbon bars and honeycomb sandwich bulkheads. The aircraft can be equipped with the engine ROTAX 912is fuel injected (100 HP) installed on the front fireproof bulkhead or with the ROTAX 912ULS (100 HP) engine. The fuel tank capacity is 50L. Version with wing-tanks of total capacity 70L (2x35L) is also available. The dashboard can be equipped with a complete set of standard flight and engine monitoring instruments. Upholstered pilot seat is made of ergonomically shaped PU foam.
Tailplanes in classical arrangement are integral part of the fuselage. Its strong structure assures carbon composite sandwich with NOMEX honeycomb. The elevator is controlled by pushrods and can be electrically trimmed. The rudder is controlled by stainless steel wire cable.
Trapezoidal wings with SM 701 profile are attached on the CrMo center wing made of CrMo steel. Ailerons and flaps are controlled by pushrods. The flaps are electrically controlled from neutral to three flap positions.
The landing gear is in classical configuration with steerable tail wheel. The main gear is designed as a pair of leaf composite springs. The size of the main gear wheels is 350 x 120 mm. The wheels are fitted with hydraulic brakes and are covered by aerodynamic spats.
By its performance, maneuverability and strength, the ATEC 212 SOLO is over standard design requirements for the ultralight category.
SPECIFICATIONS
Wingspan
24' 6"
Length
17' 0"
Height
5' 0"
Wing Area
23.85 sqft
Tailspan
7' 2"
Min. empty weight (Rotax 912uls, central fuel tank)
518 lbs.
Max. take-off weight
827 lbs.
Fuel capacity (central tank / wing tanks)
13 gal. / 2 x 9.25 gal.
PERFORMANCE
Rotax 912 (100 hp)
Cruising Speed
140 kts
Never exceed speed
167 kts
Stall speed (flaps extended)
27 kts
Stall speed (flaps retracted)
38 kts
Max. horizontal speed
157 kts
Rate of climb
1680 FPM
G-load limit
+6 / -4
Flight Range
560 nm
Fuel consumption
4.5 gph
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