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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
8
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gptkbp:bfsParent
|
gptkb:Grob_Tutor_II
|
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gptkbp:aircraft_operated
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gptkb:aircraft
high-wing
68 kg/m²
|
|
gptkbp:avionics
|
basic avionics package
|
|
gptkbp:capacity
|
2
|
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gptkbp:cockpit
|
tandem seating
|
|
gptkbp:controls
|
dual controls
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
primary trainer
|
|
gptkbp:emergency_services
|
good emergency landing characteristics
|
|
gptkbp:engine
|
Rotax 912
|
|
gptkbp:financial_performance
|
good stability characteristics
|
|
gptkbp:first_flight
|
gptkb:1985
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
all-moving tailplane
|
|
gptkbp:fuel_capacity
|
100 L
|
|
gptkbp:height
|
2.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob G 115
|
|
gptkbp:is_adept_at
|
limited acrobatic capability
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:market
|
gptkb:1985
general aviation
|
|
gptkbp:marketed_as
|
Grob G 115 E
|
|
gptkbp:material
|
composite materials
monocoque construction
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
850 kg
|
|
gptkbp:notable_ships
|
conventional rudder
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:produced_by
|
1985-1995
|
|
gptkbp:propulsion
|
variable-pitch propeller
0.25 k W/kg
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirement_year
|
gptkb:1995
|
|
gptkbp:safety_features
|
crash-resistant fuel system
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:successor
|
gptkb:Grob_G_120
|
|
gptkbp:training
|
flight training
aerobatic training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Grob G 115 D
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|