Lucas L11
{{Short description|French ultralight aircraft}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
| {{Infobox aircraft begin
| name=L11 | image= | caption= }}{{Infobox aircraft type | type=Ultralight aircraft | national origin=France | manufacturer= | designer=Emile Lucas | first flight= | introduced= | retired= | status=Plans available | primary user= | more users= | produced= | number built= | developed from= | variants with their own articles= }} |
The Lucas L11 is a French ultralight aircraft that was designed by Emile Lucas. The aircraft is supplied in the form of plans for amateur construction.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 46. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 46. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
Design and development
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.
The aircraft is made from sheet aluminum with its windshield made from a single piece of flat plastic to save money on construction costs. Access to the cockpit is via gull-winged doors. Its {{convert|8.40|ft|1|abbr=on}} span wing has an area of {{convert|9.00|m2|sqft|abbr=on}} and is equipped with flaps. The standard recommended engine is the {{convert|85|hp|kW|0|abbr=on}} Jabiru 2200 four-stroke powerplant.
Variants
Specifications (L11)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.40
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=9.00
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=275
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|80|L}}
|more general=
|eng1 number=1
|eng1 name=Jabiru 2200
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=85
|prop blade number=2
|prop name=composite
|prop dia m=
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|prop dia in=
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|perfhide=
|max speed kmh=203
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=180
|cruise speed mph=
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|cruise speed note=
|stall speed kmh=65
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
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|ceiling m=
|ceiling ft=
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|climb rate ms=5
|climb rate ftmin=
|climb rate note=
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}}
References
{{reflist}}
External links
- {{Official website|http://www.emile-lucas.com/}}
{{Lucas aircraft}}
Category:2000s French ultralight aircraft