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139:. Engines in the 80 to 120 hp (60 to 89 kW) can be used. The Highlander was designed for, but never approved for
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microlight rules. It features a biplane wing configuration, a two-seats-in-
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100 litres (22 imp gal; 26 US gal) in two tanks
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and wooden-framed 7.3 m (24.0 ft) span wings with
267:, page 23. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
429:1990s Czech and Czechoslovak ultralight aircraft
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378:This article on an aircraft of the 1990s is a
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109:The aircraft was designed to comply with the
285:, page 24. Flying Pages Europe SARL, 2015.
265:World Directory of Leisure Aviation 2011-12
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283:World Directory of Light Aviation 2015-16
263:Bayerl, Robby; Martin Berkemeier; et al:
219:188 km/h (117 mph, 102 kn)
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111:Fédération Aéronautique Internationale
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281:Tacke, Willi; Marino Boric; et al:
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180:7.3 m (23 ft 11 in)
93:that was designed and produced by
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186:14.5 m (156 sq ft)
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444:Single-engined tractor aircraft
237:10 m/s (2,000 ft/min)
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128:The aircraft has a composite
382:. You can help Knowledge by
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147:Specifications (Highlander)
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198:450 kg (992 lb)
192:240 kg (529 lb)
119:conventional landing gear
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137:aircraft fabric covering
16:Czech ultralight biplane
159:General characteristics
121:and a single engine in
105:Design and development
101:, introduced in 1998.
123:tractor configuration
73:Production completed
454:1990s aircraft stubs
117:open cockpit, fixed
339:Ultralight aircraft
31:Ultralight aircraft
434:Homebuilt aircraft
81:AirLony Highlander
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34:Type of aircraft
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210:Performance
22:Highlander
423:Categories
352:Skylane UL
347:Highlander
244:References
184:Wing area:
141:aerobatics
88:ultralight
291:1368-485X
178:Wingspan:
172:Capacity:
152:Data from
449:Biplanes
332:aircraft
130:fuselage
330:AirLony
95:AirLony
91:biplane
70:Status
56:AirLony
289:
154:Bayerl
115:tandem
166:Crew:
134:doped
99:Štětí
85:Czech
83:is a
65:1998
27:Role
380:stub
287:ISSN
79:The
168:one
97:of
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