- Design and development
- Specifications (212 Solo)
- References
- External links
| name=212 Solo | image= | caption= }}{{Infobox Aircraft Type | type=Ultralight aircraft | national origin=Czech Republic | manufacturer=ATEC v.o.s. | designer= | first flight= | introduced= | retired= | status=In production | primary user= | more users= | produced= | number built= | program cost= | unit cost= €43,225 (2015) | developed from= | variants with their own articles=
}} |
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] Design and developmentThe aircraft was designed to comply with the Fédération Aéronautique 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 {{convert|7.48|m|ft|1|abbr=on}} span wing employs an SM701 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.[1][2] Specifications (212 Solo) {{Aircraft specs
|ref=Bayerl[1][2]
|prime units?=met
|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=
|eng1 number=1
|eng1 name=Rotax 582
|eng1 type=twin cylinder, liquid-cooled, two stroke
|eng1 kw=48
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|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=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|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=
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|avionics=
}}
References1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 28. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 29. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
External links{{commons category|ATEC}}- {{Official website|http://www.atecaircraft.eu/en/planes/solo/}}
{{ATEC aircraft}} 3 : Czech ultralight aircraft 2000–2009|Single-engined tractor aircraft|ATEC aircraft |