About: AeroAndina MXP-1000 Tayrona

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The Aeroandina MXP-1000 Tayrona is a single engine, high wing, two seat ultralight, based on the Zenair formula, developed in Colombia by AeroAndina. It was launched in 2005.

Attributes	Values
rdf:type	Thing software schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	AeroAndina MXP-1000 Tayrona (en)
rdfs:comment	The Aeroandina MXP-1000 Tayrona is a single engine, high wing, two seat ultralight, based on the Zenair formula, developed in Colombia by AeroAndina. It was launched in 2005. (en)
dcterms:subject	2000s Colombian aircraft
Wikipage page ID	34120290 (xsd:integer)
Wikipage revision ID	993809036 (xsd:integer)
Link from a Wikipage to another Wikipage	Rotax 914 Ultralight dbr:Aeroandinas_MXP-800_Fantasy Rotax 914 ULS Turbo Colombia Fuselage Leading edge AMD AMD Patriot AeroAndina Europe Fin Tayrona National Natural Park Flap (aircraft) Flaperons 2000s Colombian aircraft Chord (aircraft) Cockpit Tailplane Fairing (aircraft) Cantilever Rudder Zenair High wing Rotax 912UL Tricycle undercarriage Flat-four Rotax 912ULS Side-by-side configuration Leading edge slat Jury strut Lift strut Zenair CH 701
Link from a Wikipage to an external page	https://web.archive.org/web/20100503141230/http:/www.aeroandina.com:80/eng/1000.htm
sameAs	AeroAndina MXP-1000 Tayrona AeroAndina MXP-1000 Tayrona AeroAndina MXP-1000 Tayrona AeroAndina MXP-1000 Tayrona
span m	10 (xsd:integer)
stall speed kmh	56 (xsd:integer)
stall speed note	flaps down (en)
wing area note	gross (en)
wing area sqm	12.230000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Infobox_aircraft_type dbt:Reflist dbt:AeroAndina_aircraft dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	c.2005 (en)
national origin	Colombia
capacity	one passenger (en)
crew	one (en)
fuel capacity	92 (xsd:integer)
manufacturer	AeroAndina
ref	Jane's All the World's Aircraft 2011/12 (en)
type	Two seat ultralight (en)
has abstract	The Aeroandina MXP-1000 Tayrona is a single engine, high wing, two seat ultralight, based on the Zenair formula, developed in Colombia by AeroAndina. It was launched in 2005. (en)
ceiling m	3660 (xsd:integer)
climb rate ms	5.600000 (xsd:double)
climb rate note	maximum at sea level (en)
cruise speed kmh	190 (xsd:integer)
cruise speed note	at 75% power (en)
developed from	dbr:Aeroandinas_MXP-800_Fantasy
empty weight kg	290 (xsd:integer)
eng1 kw	84.600000 (xsd:double)
eng1 name	Rotax 914 ULS Turbo
g limits	+6/-3 (en)
height m	2.400000 (xsd:double)
length m	6.300000 (xsd:double)
max speed kmh	200 (xsd:integer)
max takeoff weight kg	640 (xsd:integer)
more performance	3600.0 (second)
never exceed speed kmh	230 (xsd:integer)
number built	more than 26 (en)
prop blade number	2 (xsd:integer)
prop name	ground adjustable pitch (en)
range km	1046 (xsd:integer)
range note	at 75% power (en)
gold:hypernym	Engine

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