Jodel D18
{{Short description|French ultralight aeroplane}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
{{Infobox aircraft begin
| name=D18 & D19 | image=Jodel D18, Private JP7611653.jpg | caption=Jodel D18 }}{{Infobox aircraft type | type=Ultralight aircraft | national origin=France | manufacturer=Jodel | designer= | first flight= | introduced= | retired= | status=In production | primary user= | more users= | produced= | number built= | developed from= | variants with their own articles= }} |
The Jodel D18 is a French ultralight aircraft, designed and produced by Jodel.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 31. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 32. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 122. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}
Design and development
The original amateur-built category D18 was adapted to comply with the Fédération Aéronautique Internationale microlight rules with the addition of larger flaps and renamed the D185. Both the D18 and D185 feature a cantilever low wing, two seats in a side-by-side enclosed cockpit configuration, fixed conventional landing gear and a single engine in tractor configuration.
A tricycle landing gear-equipped version is designated D19 for the amateur-built category and D195 for the microlight category.
All the aircraft in the series are all made with a wooden structure, covered in doped aircraft fabric. The {{convert|7.50|m|ft|1|abbr=on}} span wing employs polyhedral configuration with the outer wing panels exhibiting much greater dihedral. Engines used include the {{convert|85|hp|kW|0|abbr=on}} Jabiru 2200 four-stroke powerplant as well as Rotax, Limbach Flugmotoren and {{convert|58|hp|kW|0|abbr=on}} Volkswagen 1600 automotive engines.
Variants
File:Resch Jodel D.18 Exp. AN1693807.jpg
;D18
:Original design for the amateur-built category.
;D185
:Model with tailwheel landing gear and larger flaps for the European microlight category.
;D19
:Model with tricycle landing gear for the amateur-built category.
;D195
:Model with tricycle landing gear and larger flaps for the European microlight category.
Specifications (D185)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=7.50
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=10.5
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=230
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|65|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=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=235
|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=60
|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=6
|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=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References
{{reflist}}
External links
{{commons category|Jodel D18}}
- {{Official website|http://www.avionsjodel.com/}}
{{Jodel aircraft}}
Category:1980s French ultralight aircraft