- Design and development
- Specifications (MXP-158 Embera)
- References
| name=MXP-158 Embera | image= | caption= }}{{Infobox Aircraft Type | type=Ultralight aircraft | national origin=Colombia | manufacturer=AeroAndina | designer= | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= | number built= | program cost= | unit cost= €41,196 (2011) | developed from= AeroAndina MXP-150 Kimbaya | variants with their own articles=
}} |
The AeroAndina MXP-158 Embera is a Colombian ultralight aircraft that was designed and produced by AeroAndina of Cali. The aircraft was available ready-to fly.[1] The MXP-158 is no longer in production.[2] Design and developmentThe aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and is noted for its robust design and ability to handle rough field operations. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, tricycle landing gear and a single engine in tractor configuration.[1] The aircraft is made from aluminum sheet. Its {{convert|9.5|m|ft|1|abbr=on}} span wing is supported by V-struts and jury struts. The standard engine available was the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant.[1] Specifications (MXP-158 Embera) {{Aircraft specs
|ref=Bayerl[1]
|prime units?=met
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|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=
|span in=
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=11.7
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=279
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|87|l}}
|more general=
|eng1 number=1
|eng1 name=Rotax 912UL
|eng1 type=four cylinder, liquid and air-cooled, four stroke
|eng1 kw=
|eng1 hp=80
|prop blade number=3
|prop name=composite
|prop dia m=
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|max speed kmh=190
|max speed mph=
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|cruise speed kmh=175
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|stall speed kmh=54
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|ceiling m=
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|climb rate ms=5.2
|climb rate ftmin=
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References1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 16. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^{{cite web|url=http://www.aeroandina.com/eng/modelos.htm |title=Our Models |accessdate=17 April 2012 |last=AeroAndina |date=n.d. |deadurl=yes |archiveurl=https://web.archive.org/web/20120131121225/http://www.aeroandina.com/eng/modelos.htm |archivedate=31 January 2012 |df= }}
{{AeroAndina aircraft}} 2 : Colombian ultralight aircraft 1990-1999|Single-engined tractor aircraft |