^ abcdBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 28. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
^ abcdTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 29. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External linksEdit
Official website
October 21, 2023
atec, solo, czech, ultralight, aircraft, designed, produced, atec, libice, cidlinou, aircraft, supplied, complete, ready, aircraft, solorole, ultralight, aircraftnational, origin, czech, republicmanufacturer, atec, status, production, contents, design, develop. The ATEC 212 Solo is a Czech ultralight aircraft designed and produced by ATEC v o s of Libice nad Cidlinou The aircraft is supplied as a complete ready to fly aircraft 1 2 212 SoloRole Ultralight aircraftNational origin Czech RepublicManufacturer ATEC v o s Status In production Contents 1 Design and development 2 Specifications 212 Solo 3 References 4 External linksDesign and development EditThe aircraft was designed to comply with the Federation Aeronautique Internationale microlight rules It features a cantilever low wing a single seat enclosed cockpit with a bubble canopy fixed conventional landing gear and a single engine in tractor configuration 1 2 The 212 Solo is made from carbon fibre and was derived from the ATEC 321 Faeta and ATEC 122 Zephyr 2000 designs Its 7 48 m 24 5 ft span wing employs an SM701 airfoil and slotted flaps Standard engines available are the 64 hp 48 kW Rotax 582 two stroke and the 80 hp 60 kW Rotax 912UL four stroke powerplant 1 2 Specifications 212 Solo EditData from Bayerl 1 2 General characteristicsCrew one Wingspan 7 48 m 24 ft 6 in Wing area 7 27 m2 78 3 sq ft Empty weight 200 kg 441 lb Gross weight 315 kg 694 lb Fuel capacity 50 litres 11 imp gal 13 US gal Powerplant 1 Rotax 582 twin cylinder liquid cooled two stroke 48 kW 64 hp Propellers 3 bladed compositePerformance Maximum speed 250 km h 160 mph 130 kn Cruise speed 220 km h 140 mph 120 kn Stall speed 65 km h 40 mph 35 kn Rate of climb 7 m s 1 400 ft min Wing loading 43 32 kg m2 8 87 lb sq ft References Edit a b c d Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 28 WDLA UK Lancaster UK 2011 ISSN 1368 485X a b c d Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 29 Flying Pages Europe SARL 2015 ISSN 1368 485XExternal links EditOfficial website Retrieved from https en wikipedia org w index php title ATEC 212 Solo amp oldid 1113333521, wikipedia, wiki, book, books, library,
