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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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single engine
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gptkbp:aircraft_operated
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gptkb:light_aircraft
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gptkbp:aircraft_type
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gptkb:training
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gptkbp:cockpit
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glass cockpit
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gptkbp:controls
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dual control
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gptkbp:crew
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gptkb:1
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gptkbp:design
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gptkb:Burkhard_Grob
low-wing monoplane
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gptkbp:engine
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Rotax 912
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gptkbp:engine_type
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piston engine
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gptkbp:first_flight
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gptkb:1999
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gptkbp:flaps
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split flaps
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gptkbp:fuel_capacity
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120 L
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gptkbp:height
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2.4 m
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https://www.w3.org/2000/01/rdf-schema#label
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Grob G 120
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gptkbp:introduced
|
gptkb:2000
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gptkbp:landing_gear
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tricycle gear
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gptkbp:length
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8.1 m
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gptkbp:manufacturer
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gptkb:Grob_Aircraft
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gptkbp:market
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gptkb:civil_aviation
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gptkbp:max_speed
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200 km/h
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gptkbp:max_takeoff_weight
|
1,200 kg
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gptkbp:notable_users
|
flight schools
private owners
aerobatic teams
military training units
aeronautical universities
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gptkbp:offers_certificate
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gptkb:EASA_CS-23
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gptkbp:passenger_capacity
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2
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gptkbp:produces
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ongoing
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gptkbp:production_location
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gptkb:Germany
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gptkbp:propeller
|
variable pitch
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gptkbp:range
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1,000 km
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gptkbp:role
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gptkb:trainer_aircraft
gptkb:light_aircraft
|
|
gptkbp:safety_record
|
generally safe
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gptkbp:service_ceiling
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4,500 m
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gptkbp:stall_speed
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65 km/h
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gptkbp:trademark
|
Grob
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gptkbp:variant
|
gptkb:G_120_TP
G 120 A
G 120 C
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gptkbp:weight
|
750 kg
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gptkbp:wing_area
|
14.5 m²
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gptkbp:wingspan
|
10.5 m
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gptkbp:bfsParent
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gptkb:Luftwaffe
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gptkbp:bfsLayer
|
4
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