Bilsam Sky Walker II

{{Short description|Polish powered parachute}}

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

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

{{Infobox aircraft begin

| name= Sky Walker II

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| type=Powered parachute

| national origin=Poland

| manufacturer=Bilsam Aviation

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The Bilsam Sky Walker II is a Polish powered parachute designed and produced by Bilsam Aviation of Poznań. The aircraft is supplied as a complete ready-to-fly-aircraft.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 80. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X

Design and development

The Sky Walker II is very different from the company's Sky Walker I and 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|400|kg|lb|0|abbr=on}}. It features a {{convert|50|m2|sqft|abbr=on}} parachute-style wing, two-seats-in-side-by-side configuration, tricycle landing gear and a single {{convert|60|hp|kW|0|abbr=on}} Bilsam TNA 625 four stroke engine in pusher configuration.

The aircraft carriage is built from a combination of composite material and steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. Unusually for this class of aircraft, the Sky Walker II has an enclosed cockpit. A variety of wings can be fitted.

The aircraft has an empty weight of {{convert|155|kg|lb|0|abbr=on}} and a gross weight of {{convert|400|kg|lb|0|abbr=on}}, giving a useful load of {{convert|245|kg|lb|0|abbr=on}}. With full fuel of {{convert|40|L}} the payload for crew and baggage is {{convert|216|kg|lb|0|abbr=on}}.

Specifications (Sky Walker II)

{{Aircraft specs

|ref=Bertrand

|prime units?=met

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|crew=one

|capacity=one passenger

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|aspect ratio=4.5:1

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|empty weight kg=155

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|gross weight kg=400

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|fuel capacity={{convert|40|L}}

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|eng1 number=1

|eng1 name=Bilsam TNA 625

|eng1 type=four-stroke, air-cooled aircraft engine

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|eng1 hp=60

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|max speed kmh=48

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|cruise speed kmh=40

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|stall speed kmh=16

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|wing loading kg/m2=8.0

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}}

References

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