|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
straight wing
|
|
gptkbp:airlines
|
yes
1 pilot
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:communicationEquipment
|
VHF radio
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
Hirth HM 504
|
|
gptkbp:enginePower
|
150 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1945
|
|
gptkbp:floors
|
tailplane
|
|
gptkbp:fuelCapacity
|
150 L
|
|
gptkbp:headlights
|
metal
PH-XXX
|
|
gptkbp:height
|
2.60 m
|
|
gptkbp:historicalSignificance
|
used in military training
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fokker S.11
|
|
gptkbp:introduced
|
1948
|
|
gptkbp:landingGear
|
tricycle gear
retractable landing gear
|
|
gptkbp:layout
|
conventional layout
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fokker
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:missions
|
manual control
|
|
gptkbp:nationalTeam
|
gptkb:Netherlands
|
|
gptkbp:navigationEquipment
|
basic navigation instruments
|
|
gptkbp:numberBuilt
|
approximately 200
|
|
gptkbp:passengerCapacity
|
none
|
|
gptkbp:primaryUser
|
gptkb:Royal_Netherlands_Air_Force
|
|
gptkbp:productionYears
|
1945-1956
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
trainer aircraft
aerobatic training
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:steering
|
fin and rudder
|
|
gptkbp:succeededBy
|
4.5°/s
|
|
gptkbp:supportRole
|
basic flight training
|
|
gptkbp:type
|
civilian aircraft
|
|
gptkbp:variant
|
Fokker_S.11_Instructor
|
|
gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.50 m
|