About: TL Ultralight TL-32 Typhoon     Goto   Sponge   NotDistinct   Permalink

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The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s.

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rdf:type
rdfs:label
  • TL Ultralight TL-32 Typhoon (en)
rdfs:comment
  • The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s. (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/OK-OUR-15_TL-32_Day.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/OK-OUR-15_TL-32_Night.jpg
dcterms:subject
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span m
stall speed kmh
wing area note
  • gross (en)
wing area sqm
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thumbnail
dbp:primeUnits%3F_
  • met (en)
national origin
capacity
introduced
manufacturer
ref
  • Jane's All the World's Aircraft 2000/01 (en)
type
  • Two seat ultralight (en)
has abstract
  • The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s. (en)
cruise speed kmh
empty weight kg
eng1 name
  • Rotax (en)
eng1 number
eng1 type
  • two cylinder two stroke (en)
height m
length m
max speed kmh
max takeoff weight kg
number built
  • More than 200 (en)
range km
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page length (characters) of wiki page
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origin
type
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is Link from a Wikipage to another Wikipage of
is foaf:primaryTopic of
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