gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_color
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various colors available
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gptkbp:aircraft_configuration
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conventional configuration
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gptkbp:aircraft_features
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high visibility cockpit
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gptkbp:aircraft_operated
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gptkb:training
gptkb:light_aircraft
advanced avionics
easy maintenance access
aerobatics training
500 kg empty weight
part of Grob's legacy in aviation.
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gptkbp:aircraft_performance
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good climb rate
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gptkbp:aircraft_reputation
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well-regarded in training circles
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gptkbp:capacity
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2
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gptkbp:cockpit
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two-seat cockpit
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gptkbp:control_surfaces
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gptkb:elevator
rudder
aileron
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gptkbp:country_of_origin
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gptkb:Germany
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gptkbp:crew
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gptkb:1
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gptkbp:design
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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:first_flight
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gptkb:1980
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gptkbp:flaps
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split flaps
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gptkbp:fuel_capacity
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100 L
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gptkbp:fuselage_material
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composite materials
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gptkbp:height
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2.1 m
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https://www.w3.org/2000/01/rdf-schema#label
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Grob Tutor IIe
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gptkbp:introduced
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gptkb:1980
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gptkbp:landing_gear
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tricycle gear
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gptkbp:length
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7.2 m
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gptkbp:manufacturer
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gptkb:Grob_Aircraft
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gptkbp:max_speed
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200 km/h
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gptkbp:max_takeoff_weight
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600 kg
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gptkbp:notable_users
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various flying schools
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gptkbp:number_built
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over 200
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gptkbp:offers_certificate
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gptkb:EASA
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gptkbp:operational_range
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long range
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gptkbp:propeller
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variable-pitch propeller
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gptkbp:propulsion
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propeller-driven
0.1 k W/kg
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gptkbp:range
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800 km
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gptkbp:role
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gptkb:trainer_aircraft
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gptkbp:service_ceiling
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4,000 m
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gptkbp:stall_characteristics
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docile stall characteristics
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gptkbp:stall_speed
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60 km/h
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gptkbp:successor
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Grob 120
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gptkbp:tail_type
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T-tail
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gptkbp:training
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basic flight training
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gptkbp:trim_system
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manual trim
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gptkbp:used_in
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pilot training
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gptkbp:wing_area
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12.5 m²
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gptkbp:wing_configuration
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cantilever wing
48 kg/m²
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gptkbp:wingspan
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9.5 m
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gptkbp:bfsParent
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gptkb:Grob_Tutor_II
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gptkbp:bfsLayer
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8
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