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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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civil aviation
conventional tail
biplane wings
aerobatic trainer
42 kg/m²
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gptkbp:cockpit
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open cockpit
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gptkbp:constructionMaterial
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wood and fabric
NACA 2412
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gptkbp:controls
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ailerons
elevator
rudder
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gptkbp:countryOfOrigin
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gptkb:Germany
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gptkbp:crew
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1
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gptkbp:currentStatus
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some still flying
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gptkbp:design
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gptkb:Carl_Bücker
highly maneuverable
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gptkbp:engine
|
Hirth HM 504
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gptkbp:engineType
|
inline engine
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gptkbp:famousFor
|
Europe
aerobatic capabilities
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gptkbp:firstFlight
|
1934
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gptkbp:fuelCapacity
|
50 L
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gptkbp:headlights
|
conventional tail
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gptkbp:height
|
2.3 m
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gptkbp:historicalSignificance
|
popular in flight schools
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|
https://www.w3.org/2000/01/rdf-schema#label
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Bücker Jungmann
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gptkbp:influencedBy
|
gptkb:Bücker_Bü_131
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gptkbp:introduced
|
1934
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gptkbp:landingGear
|
tailwheel
|
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gptkbp:length
|
7.0 m
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|
gptkbp:manufacturer
|
gptkb:Bücker_Flugzeugbau
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|
gptkbp:maxSpeed
|
200 km/h
|
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gptkbp:maxTakeoffWeight
|
650 kg
|
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gptkbp:notableFeature
|
gptkb:Hermann_Göring
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gptkbp:numberBuilt
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approximately 1,000
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gptkbp:passengerCapacity
|
1
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gptkbp:productionLocation
|
gptkb:Germany
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gptkbp:productionYears
|
1934-1949
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gptkbp:propulsion
|
0.1 kW/kg
|
|
gptkbp:rateOfFire
|
5.5 m/s
|
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gptkbp:relatedAircraft
|
gptkb:Bücker_Jungmeister
|
|
gptkbp:retirementYear
|
1960s
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gptkbp:role
|
trainer aircraft
used in aerobatic competitions
|
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gptkbp:services
|
4,000 m
|
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gptkbp:speed
|
60 km/h
|
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gptkbp:successor
|
gptkb:Bücker_Bü_180
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|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:Luftwaffe
|
|
gptkbp:usedIn
|
airshows
|
|
gptkbp:variant
|
gptkb:Bücker_Jungmeister
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:wingArea
|
15.5 m²
|
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gptkbp:wingspan
|
8.2 m
|