About: Roko Aero NG4

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The Roko Aero NG4 is a single-engined sport aircraft, available in both light-sport aircraft and ultralight models, which seats two side by side. It is in production in the Czech Republic.

Attributes	Values
rdf:type	Thing 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	Roko Aero NG4 (en)
rdfs:comment	The Roko Aero NG4 is a single-engined sport aircraft, available in both light-sport aircraft and ultralight models, which seats two side by side. It is in production in the Czech Republic. (en)
foaf:depiction
dcterms:subject	Ultralight aircraft 2000s Czech sport aircraft Low-wing aircraft Light-sport aircraft Single-engined tractor aircraft Aircraft first flown in 2008
Wikipage page ID	31287412 (xsd:integer)
Wikipage revision ID	993820340 (xsd:integer)
Link from a Wikipage to another Wikipage	Rotax 914 Monoplane Ultralight Light-sport aircraft GPS Ultralight aircraft 2000s Czech sport aircraft Composite material Zlin Trim tab Wheel spats Low-wing aircraft CZAW SportCruiser Ailerons Light-sport aircraft Single-engined tractor aircraft Czech Republic Flap (aircraft) Aircraft first flown in 2008 Jabiru 2200 Wing configuration Visual flight rules Rotax 912 ULS Rotax 912 UL Tricycle gear Czech Aircraft Works EFIS Rotax 912ULS Continental IO-240
sameAs	Roko Aero NG4 Roko Aero NG4 Roko Aero NG4
span m	10.100000 (xsd:double)
stall speed kmh	55 (xsd:integer)
stall speed note	flaps down (en)
wing area note	gross (en)
wing area sqm	13 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Refbegin dbt:Refend dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Roko_Aero_NG4_UL_AN1569070.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	2008-03-23 (xsd:date)
national origin	Czech Republic
capacity	1 (xsd:integer)
crew	1 (xsd:integer)
designer	Jiří Konečný (en)
fuel capacity	130.0 (litre)
introduced	2008 (xsd:integer)
manufacturer	Aero Roko A.S., Zlin (en)
ref	Jane's All the World's Aircraft 1910/11 p.176 (en)
type	Two-seat sports ultralight (en)
has abstract	The Roko Aero NG4 is a single-engined sport aircraft, available in both light-sport aircraft and ultralight models, which seats two side by side. It is in production in the Czech Republic. (en)
airfoil	MS316 at root, MS313 at tip (en)
avionics	Standard VFR AvMap EKP IV GPS *Dynon EFIS optional (en)
cruise speed kmh	240 (xsd:integer)
developed from	CZAW SportCruiser
empty weight kg	330 (xsd:integer)
eng1 hp	100 (xsd:integer)
eng1 name	Rotax 912ULS
eng1 number	1 (xsd:integer)
eng1 type	flat four water/air cooled piston (en)
g limits	+4/-2 (en)
height m	2.280000 (xsd:double)
length m	6.450000 (xsd:double)
max takeoff weight kg	600 (xsd:integer)
never exceed speed kmh	270 (xsd:integer)
number built	37 (xsd:integer)
prop blade number	3 (xsd:integer)
prop name	Woodcomp (en)
gold:hypernym	Aircraft

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