Adventure Wheely II

{{Short description|French powered parachute}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox aircraft begin

| name= Wheely II

| image=

| caption=

}}{{Infobox aircraft type

| type=Powered parachute

| national origin=France

| manufacturer=Adventure SA

| designer=

| first flight=

| introduced=

| retired=

| status=Production completed

| primary user=

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}}

The Adventure Wheely II is a French powered parachute that was designed and produced by Adventure SA of Paris. Now out of production, when it was available the aircraft was supplied as a complete ready-to-fly-aircraft.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 79. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X

Design and development

The Wheely II was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}. The aircraft has a maximum gross weight of {{convert|270|kg|lb|0|abbr=on}}. It features a {{convert|40|m2|sqft|abbr=on}} parachute-style wing, two-seats-in-tandem, tricycle landing gear and dual {{convert|14.5|hp|kW|0|abbr=on}} Solo 210 engines mounted together in pusher configuration driving a single propeller, although other engines can be used.

The aircraft carriage is built from a combination of bolted aluminium and plastics. The propeller is mounted within a two-tube safety ring, with a mesh net set forward to keep objects out of the propeller. In flight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw. The main landing gear incorporates spring rod suspension.

The aircraft has an empty weight of {{convert|70|kg|lb|0|abbr=on}} and a gross weight of {{convert|270|kg|lb|0|abbr=on}}, giving a useful load of {{convert|200|kg|lb|0|abbr=on}}. With a fuel capacity of {{convert|23|L}} the full-fuel payload for crew and baggage is {{convert|143|kg|lb|0|abbr=on}}.

Specifications (Wheely II)

{{Aircraft specs

|ref=Bertrand

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=

|length in=

|length note=

|span m=13

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=40

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=70

|empty weight lb=

|empty weight note=

|gross weight kg=270

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|23|L}}

|more general=

|eng1 number=2

|eng1 name=Solo 210

|eng1 type=single cylinder, two-stroke, air-cooled aircraft engines

|eng1 kw=

|eng1 hp=14.5

|prop blade number=2

|prop name=wooden, fixed pitch

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=55

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=55

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=25

|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=

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|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

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|glide ratio=

|climb rate ms=2

|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=6.75

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References