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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
civil aviation
|
|
gptkbp:capacity
|
10 passengers
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:countryOfOrigin
|
gptkb:Netherlands
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Hendrik_Fokker
|
|
gptkbp:enginePower
|
450 hp
|
|
gptkbp:engineType
|
radial engine
|
|
gptkbp:firstFlight
|
1929
1940
|
|
gptkbp:fuelCapacity
|
400 L
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:historicalSignificance
|
early commercial aviation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fokker S.24
|
|
gptkbp:introduced
|
1930
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
14.5 m
|
|
gptkbp:manufacturer
|
gptkb:Fokker
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,000 kg
|
|
gptkbp:notableFeature
|
high wing configuration
open cockpit
large cabin space
fixed landing gear
|
|
gptkbp:numberBuilt
|
20
|
|
gptkbp:predecessor
|
gptkb:Fokker_S.11
|
|
gptkbp:productionYears
|
1929-1930
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retired
|
1940
|
|
gptkbp:retirementYear
|
outdated technology
|
|
gptkbp:role
|
passenger transport
|
|
gptkbp:services
|
1930s
3,000 m
|
|
gptkbp:successor
|
gptkb:Fokker_F.VII
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:KLM_Royal_Dutch_Airlines
gptkb:Dutch_Air_Force
|
|
gptkbp:variant
|
Fokker S.24A
Fokker_S.24B
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wingArea
|
50 m²
|
|
gptkbp:wingspan
|
20.5 m
|