Arplast Micro'B

{{short description|French ultralight aircraft}}

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

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

{{Infobox aircraft begin

| name=Micro'B

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| type=Ultralight aircraft

| national origin=France

| manufacturer=Arplast Helice

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| status=Production completed

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The Arplast Micro'B ({{langx|en|Microbe}}) is a French ultralight aircraft that was designed and produced by propeller manufacturer Arplast Helice. It was supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 26. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The Arplast Micro'B was designed to comply with the Fédération Aéronautique Internationale microlight rules, with a lightened version for the US FAR 103 Ultralight Vehicles category. It features a strut-braced high-wing, a single-seat enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.

The Micro'B is made from a combination of welded steel and carbon fibre, with the flying surfaces made from the latter material. Its {{convert|8.6|m|ft|1|abbr=on}} span wing is supported by a single strut per side and features automatic flaps. Standard engines included the {{convert|40|hp|kW|0|abbr=on}} Rotax 447 two-stroke or other small lightweight motors, mounted on the main keel tube above the cockpit.

Variants

;Micro'B

:Initial version, which was used to win the World Microlight Championships.

;Micro'B ML

:Improved version, with carbon fibre construction for the FAI Microlight class. Standard engine supplied was the {{convert|40|hp|kW|0|abbr=on}} Rotax 447 two-stroke aircraft engine. Empty weight of {{convert|125|kg|lb|0|abbr=on}}.

;Micro'B 103

:Lightened version for the US ultralight category, equipped with a {{convert|25|hp|kW|0|abbr=on}} Briggs & Stratton V-twin engine. Empty weight of {{convert|110|kg|lb|0|abbr=on}}.

Specifications (Micro'B 103)

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References

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