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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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1,400 kg
civil and military
cantilever wing
77 kg/m²
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gptkbp:armament
|
none
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gptkbp:climbRate
|
5 m/s
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gptkbp:cockpit
|
open cockpit
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gptkbp:constructionMaterial
|
metal construction
NACA 2412
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gptkbp:covers
|
split flaps
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gptkbp:crew
|
1
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gptkbp:design
|
gptkb:Hermann_Pohlmann
low-wing monoplane
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gptkbp:engine
|
Hirth HM 508
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gptkbp:financial_aid
|
good stability and control
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gptkbp:firstFlight
|
1935
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gptkbp:floors
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balanced control surfaces
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gptkbp:fuelCapacity
|
120 L
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gptkbp:headlights
|
conventional tail
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gptkbp:height
|
2.60 m
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gptkbp:historicalSignificance
|
used_in_WWII_training_programs
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|
https://www.w3.org/2000/01/rdf-schema#label
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Focke-Wulf Fw 56
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gptkbp:influencedBy
|
Focke-Wulf Fw 44 Stieglitz
|
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gptkbp:introduced
|
1936
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gptkbp:landingGear
|
tailwheel
|
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gptkbp:length
|
8.20 m
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gptkbp:manufacturer
|
gptkb:Focke-Wulf
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gptkbp:marketedAs
|
training aircraft
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gptkbp:maxSpeed
|
220 km/h
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gptkbp:maxTakeoffWeight
|
1,200 kg
|
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gptkbp:notableUsers
|
gptkb:Austria
gptkb:Germany
gptkb:Hungary
gptkb:Spain
gptkb:Sweden
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gptkbp:numberBuilt
|
approximately 1,000
|
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gptkbp:operationalStatus
|
frise ailerons
|
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gptkbp:powers
|
160 hp
|
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gptkbp:primaryUser
|
gptkb:Luftwaffe
|
|
gptkbp:productionYears
|
1935-1945
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|
gptkbp:propulsion
|
0.13 hp/kg
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
1945
|
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gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:steering
|
effective rudder
|
|
gptkbp:succeededBy
|
3.5°/s
|
|
gptkbp:successor
|
gptkb:Focke-Wulf_Fw_190
|
|
gptkbp:supportRole
|
basic flight training
|
|
gptkbp:variant
|
gptkb:Fw_56B
Fw 56A
Fw 56C
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gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.50 m
|