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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
|
light aircraft
single-engine
civil aviation aircraft
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|
gptkbp:capacity
|
4 passengers
|
|
gptkbp:climbRate
|
3 m/s
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gptkbp:cockpit
|
open cockpit
|
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gptkbp:constructionMaterial
|
wood
|
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gptkbp:controls
|
ailerons
elevator
rudder
|
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gptkbp:countryOfOrigin
|
gptkb:Netherlands
|
|
gptkbp:crew
|
1 pilot
|
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gptkbp:design
|
gptkb:Hendrik_Fokker
high-wing monoplane
|
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gptkbp:engineType
|
radial engine
|
|
gptkbp:firstFlight
|
1929
|
|
gptkbp:fuelCapacity
|
200 liters
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:historicalSignificance
|
early commercial aviation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fokker S.26
|
|
gptkbp:influencedBy
|
gptkb:Fokker_F.VII
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
gptkb:Fokker
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notableFeature
|
open cockpit
|
|
gptkbp:numberBuilt
|
10
|
|
gptkbp:operationalHistory
|
used_in_Europe
|
|
gptkbp:productionYears
|
1929-1935
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirementYear
|
1935
|
|
gptkbp:role
|
passenger aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:services
|
1930
|
|
gptkbp:successor
|
gptkb:Fokker_S.30
|
|
gptkbp:usedBy
|
gptkb:KLM_Royal_Dutch_Airlines
|
|
gptkbp:variant
|
Fokker_S.26A
Fokker_S.26B
|
|
gptkbp:wingArea
|
20 m²
|
|
gptkbp:wingspan
|
10.5 m
|