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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
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gptkb:Uruguayan_Air_Force
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gptkbp:aircraft_operated
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general aviation
two-seat configuration
training and leisure
PPL, CPL
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gptkbp:avionics
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modern glass cockpit
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gptkbp:certification
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gptkb:EASA
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gptkbp:controls
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dual control
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gptkbp:crew
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gptkb:musical
|
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gptkbp:design
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gptkb:Grob_Aircraft_Gmb_H
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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four-stroke engine
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gptkbp:features
|
glass cockpit
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gptkbp:first_flight
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gptkb:2008
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gptkbp:first_released
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gptkb:2010
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gptkbp:fuel_capacity
|
120 L
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gptkbp:height
|
2.4 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob G120 TP
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gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
8.1 m
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gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:market
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gptkb:aircraft
|
|
gptkbp:market_segment
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gptkb:aircraft
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,200 kg
|
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gptkbp:number_built
|
over 100
|
|
gptkbp:operational_area
|
flight schools
|
|
gptkbp:origin
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gptkb:government_agency
|
|
gptkbp:performance
|
excellent maneuverability
|
|
gptkbp:production_years
|
2008-ongoing
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:regulatory_compliance
|
EASACS-23
|
|
gptkbp:role
|
pilot training
|
|
gptkbp:safety_features
|
high
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service_ceiling
|
5,500 m
|
|
gptkbp:speed
|
65 km/h
200 km/h
|
|
gptkbp:training
|
basic flight training
aerobatic training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
G120 TP-2
|
|
gptkbp:weight
|
750 kg
450 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
11.2 m
|