MSL Aero H80

H80
Role Ultralight aircraft
National origin France
Manufacturer MSL Aero
Designer Massimo Tedesco and Sebastian Lefebre
Status In production (2012)



The MSL Aero H80 is a French ultralight aircraft that was designed by Massimo Tedesco and Sebastian Lefebre and produced by MSL Aero of Limoges-Fourches.[1]

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from sheet aluminum. Its 8.60 m (28.2 ft) span wing has an area of 10.6 m2 (114 sq ft) and flaps. The wing is supported by V-struts and jury struts. Standard engines available are the 80 hp (60 kW) Rotax 912UL and the 100 hp (75 kW) Rotax 912ULS four-stroke powerplants.[1]

Variants

H80
Version with the 80 hp (60 kW) Rotax 912UL engine.[1]
H100
Version with the 100 hp (75 kW) Rotax 912ULS engine.[1]
H2O
Floatplane version.[1]
Type H
Version for the European ELA-1 category.[1]

Specifications (H80)

Data from Bayerl[1]

General characteristics

Performance

References

  1. 1 2 3 4 5 6 7 8 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 66. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

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