|
gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
light aircraft
high-wing configuration
cantilever wing
good maneuverability
sport aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:climbRate
|
3.5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
metal
|
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gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:crew
|
1
primary trainer
|
|
gptkbp:design
|
gptkb:Hermann_Pohlmann
low-wing monoplane
|
|
gptkbp:engine
|
Hirth HM 504
|
|
gptkbp:engineType
|
inline engine
|
|
gptkbp:firstFlight
|
1937
|
|
gptkbp:fuelCapacity
|
100 liters
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.60 m
|
|
gptkbp:historicalSignificance
|
training_pilots_during_WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Focke-Wulf Fw 44
|
|
gptkbp:IATA_code
|
used in aerobatic training.
|
|
gptkbp:landingGear
|
tailwheel
fixed landing gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Focke-Wulf
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:nickname
|
gptkb:Stieglitz
|
|
gptkbp:numberBuilt
|
approximately 1,000
|
|
gptkbp:powers
|
120 hp
|
|
gptkbp:productionLocation
|
gptkb:Germany
|
|
gptkbp:productionYears
|
1937-1940
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:role
|
trainer aircraft
civilian aircraft
|
|
gptkbp:services
|
3,500 m
used in various air forces
|
|
gptkbp:setting
|
single-engine
|
|
gptkbp:successor
|
gptkb:Focke-Wulf_Fw_56
|
|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:Luftwaffe
civil aviation
|
|
gptkbp:variant
|
Fw 44 Stieglitz
|
|
gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.50 m
|