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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
|
high-wing
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gptkbp:avionics
|
modern avionics
|
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gptkbp:cockpit
|
glass cockpit
|
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gptkbp:constructionMaterial
|
NACA 4412
monocoque construction
|
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gptkbp:controls
|
dual control
|
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gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
basic trainer
|
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gptkbp:engine
|
Rotax 912
|
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gptkbp:engineType
|
four-stroke engine
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gptkbp:firstFlight
|
1999
|
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gptkbp:firstGeneration
|
gptkb:Luftwaffe
|
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gptkbp:fuelCapacity
|
120 L
|
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gptkbp:headlights
|
T-tail
|
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gptkbp:height
|
2.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob G 120
|
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gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notableUsers
|
gptkb:Royal_Air_Force
gptkb:Austrian_Air_Force
gptkb:Luftwaffe
gptkb:Swiss_Air_Force
|
|
gptkbp:passengerCapacity
|
2
|
|
gptkbp:produces
|
ongoing
|
|
gptkbp:propulsion
|
variable-pitch
propeller-driven
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
pilot training
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:takeoffDistance
|
300 m
70 km/h
400 m
|
|
gptkbp:type
|
trainer aircraft
|
|
gptkbp:variant
|
gptkb:G_120B
G 120A
G 120TP
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|