About: Tapanee Pegazair-100

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The Pegazair-100 STOL is a two-seat STOL homebuilt aircraft developed in Canada by Tapanee Aviation, Inc. of Mont-Saint-Michel, Quebec.

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	Tapanee Pegazair-100 (en)
rdfs:comment	The Pegazair-100 STOL is a two-seat STOL homebuilt aircraft developed in Canada by Tapanee Aviation, Inc. of Mont-Saint-Michel, Quebec. (en)
foaf:depiction
dcterms:subject	High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft Aircraft first flown in 1991 Tapanee Aviation aircraft
Wikipage page ID	36768834 (xsd:integer)
Wikipage revision ID	1037305931 (xsd:integer)
Link from a Wikipage to another Wikipage	Canada Rotax 914 NACA airfoil Homebuilt aircraft Continental A-65 Mont-Saint-Michel, Quebec Continental O-200 Conventional landing gear STOL Fuselage High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft High-wing Aircraft first flown in 1991 Tailplane Tapanee Aviation aircraft Leading edge slot Flaperon Tapanee Levitation 4 Rotax 912UL Tapanee Aviation, Inc. Side-by-side configuration Leading edge slat Zenair CH 701 STOL Strut-braced
Link from a Wikipage to an external page	http://www.tapanee.com/Version_english/specifications.html
sameAs	Tapanee Pegazair-100 Tapanee Pegazair-100 Tapanee Pegazair-100
span ft	29 (xsd:integer)
stall speed mph	28 (xsd:integer)
variants with their own articles	Tapanee Levitation 4
wing area sqft	150 (xsd:integer)
wing loading lb/sqft	9.700000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Convert dbt:Infobox_aircraft_type dbt:Portal dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Tapanee_Aviation_aircraft
thumbnail	wiki-commons:Special:FilePath/Pegazair-100.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	June 1991 (en)
national origin	Canada
capacity	one passenger (en)
crew	one (en)
designer	Serg Dufour (en)
length ft	22 (xsd:integer)
manufacturer	Tapanee Aviation, Inc.
ref	Manufacturer and Kitplanes (en)
type	Homebuilt aircraft
has abstract	The Pegazair-100 STOL is a two-seat STOL homebuilt aircraft developed in Canada by Tapanee Aviation, Inc. of Mont-Saint-Michel, Quebec. (en)
airfoil	NACA airfoil
cruise speed mph	105 (xsd:integer)
empty weight lb	825 (xsd:integer)
eng1 hp	100 (xsd:integer)
eng1 name	Continental O-200
eng1 number	1 (xsd:integer)
eng1 type	horizontally opposed piston (en)
g limits	+6/-3.3 (en)
gross weight lb	1450 (xsd:integer)
length in	5 (xsd:integer)
never exceed speed mph	125 (xsd:integer)
range miles	630 (xsd:integer)
see also	*Tapanee Levitation 4 (en)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:Tapanee_Pegazair-100?oldid=1037305931&ns=0
page length (characters) of wiki page	6402 (xsd:nonNegativeInteger)
manufacturer	Tapanee Aviation, Inc.

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