- Design and development
- Specifications (Highlander)
- References
| name=Highlander | image= | caption= }}{{Infobox Aircraft Type | type=Ultralight aircraft | national origin=Czech Republic | manufacturer=AirLony | designer= | first flight= | introduced=1998 | retired= | status=Production completed | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles=
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The AirLony Highlander is a Czech ultralight biplane that was designed and produced by AirLony of Štětí, introduced in 1998.[1][2] Design and developmentThe aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a biplane wing configuration, a two-seats-in-tandem open cockpit, fixed conventional landing gear and a single engine in tractor configuration.[1][2] The aircraft has a composite fuselage and wooden-framed {{convert|7.3|m|ft|1|abbr=on}} span wings with doped aircraft fabric covering. Engines in the {{convert|80|to|120|hp|kW|0|abbr=on}} can be used. The Highlander was designed for, but never approved for aerobatics.[1][2] Specifications (Highlander) {{Aircraft specs
|ref=Bayerl[1]
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|crew=one
|capacity=one passenger
|length m=
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|span m=7.3
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|wing area sqm=14.5
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|empty weight kg=240
|empty weight lb=
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|gross weight kg=450
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|fuel capacity={{convert|100|l}} in two tanks
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|max speed kmh=188
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|cruise speed kmh=160
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|stall speed kmh=65
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|climb rate ms=10
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References1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 23. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 24. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
{{Airlony aircraft}}{{aero-1990s-stub}} 5 : Czech and Czechoslovakian ultralight aircraft 1990–1999|Homebuilt aircraft|AirLony aircraft|Single-engined tractor aircraft|Biplanes |