MSL Aero H80

Last updated

H80
Role Ultralight aircraft
National origin France
Manufacturer MSL Aero
DesignerMassimo Tedesco and Sebastian Lefebre
StatusProduction completed

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] [2]

Contents

The company seem to have gone out of business in early 2015 and production ended. [3]

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] [2]

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] [2]

Variants

H80
Version with the 80 hp (60 kW) Rotax 912UL engine. [1] [2]
H100
Version with the 100 hp (75 kW) Rotax 912ULS engine. [1] [2]
H2O
Floatplane version. [1] [2]
Type H
Version for the European ELA-1 category. [1] [2]

Specifications (H80)

Data from Bayerl and Tacke [1] [2]

General characteristics

Performance

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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
  2. 1 2 3 4 5 6 7 8 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 69. Flying Pages Europe SARL, 2015. ISSN   1368-485X
  3. ↑ "MSL Aero". Internet Archive Wayback Machine. Retrieved 2 March 2017.
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