View source for Engineering:ATEC 212 Solo

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{|{{Infobox Aircraft Begin
 | name=212 Solo
 | image=
 | caption=
}}{{Infobox Aircraft Type
 | type=Ultralight aircraft
 | national origin=[[Place:Czech Republic|Czech Republic]]
 | manufacturer=[[Company:ATEC v.o.s.|ATEC v.o.s.]]
 | designer=
 | first flight=
 | introduced=
 | retired=
 | status=In production
 | primary user=
 | more users= <!--Limited to three in total; separate using <br /> -->
 | produced= <!--years in production-->
 | number built=
 | program cost= <!--Total program cost-->
 | unit cost= [[Finance:Euro|€]]43,225 (2015)
 | developed from= 
 | variants with their own articles=
}}
|}
The '''ATEC 212 Solo''' is a [[Place:Czech Republic|Czech]] ultralight aircraft, designed and produced by [[Company:ATEC v.o.s.|ATEC v.o.s.]] of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 28. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref><ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', page 29. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref>

==Design and development==
The aircraft was designed to comply with the [[Organization:Fédération Aéronautique Internationale|Fédération Aéronautique Internationale]] microlight rules. It features a cantilever low-wing, a single-seat, enclosed cockpit with a bubble canopy, fixed [[Engineering:Conventional landing gear|conventional landing gear]] and a single engine in [[Engineering:Tractor configuration|tractor configuration]].<ref name="WDLA11" /><ref name="WDLA15"/>

The 212 Solo is made from carbon fibre and was derived from the [[Engineering:ATEC 321 Faeta|ATEC 321 Faeta]] and [[Engineering:ATEC 122 Zephyr 2000|ATEC 122 Zephyr 2000]] designs. Its {{convert|7.48|m|ft|1|abbr=on}} span wing employs an SM701 [[Physics:Airfoil|airfoil]] and slotted flaps. Standard engines available are the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke and the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant.<ref name="WDLA11" /><ref name="WDLA15"/>
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==Specifications (212 Solo) ==
{{Aircraft specs
|ref=Bayerl<ref name="WDLA11" /><ref name="WDLA15"/>
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
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        General characteristics
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|genhide=

|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=7.48
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=7.27
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=200
|empty weight lb=
|empty weight note=
|gross weight kg=315
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|50|L}}
|more general=
<!--
        Powerplant
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|eng1 number=1
|eng1 name=Rotax 582
|eng1 type=twin cylinder, liquid-cooled, two stroke
|eng1 kw=48<!-- prop engines -->
|eng1 hp=<!-- prop engines -->

|prop blade number=3<!-- propeller aircraft -->
|prop name=composite
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop note=

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        Performance
-->
|perfhide=

|max speed kmh=250
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=220
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=7
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=43.32
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

==References==
{{reflist}}

==External links==

[[Category:Single-engined tractor aircraft]]

{{Sourceattribution|ATEC 212 Solo}}