Arplast Micro'B

Micro'B
Role Ultralight aircraft
National origin France
Manufacturer Arplast Helice
Status Production completed
Unit cost
€39,000 (103 model, assembled, 2011)

The Arplast Micro'B (English: 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.[1]

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.[1]

The Micro'B is made from a combination of welded steel and carbon fibre, with the flying surfaces made from the latter material. Its 8.6 m (28.2 ft) span wing is supported by a single strut per side and features automatic flaps. Standard engines included the 40 hp (30 kW) Rotax 447 two-stroke or other small lightweight motors, mounted on the main keel tube above the cockpit.[1]

Variants

Micro'B
Initial version, which was used to win the World Microlight Championships.[1]
Micro'B ML
Improved version, with carbon fibre construction for the FAI Microlight class. Standard engine supplied was the 40 hp (30 kW) Rotax 447 two-stroke aircraft engine. Empty weight of 125 kg (276 lb).[1]
Micro'B 103
Lightened version for the US ultralight category, equipped with a 25 hp (19 kW) Briggs & Stratton V-twin engine. Empty weight of 110 kg (243 lb).[1]

Specifications (Micro'B 103)

Data from Bayerl[1]

General characteristics

Performance

References

  1. 1 2 3 4 5 6 7 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 26. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
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