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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:light_aircraft
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gptkbp:aircraft_role
|
trainer and recreational flying
|
|
gptkbp:aircraft_type
|
single-engine aircraft
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|
gptkbp:avionics
|
basic flight instruments
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gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
two-seat cockpit
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
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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
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gptkbp:design_date
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gptkb:1984
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gptkbp:design_feature
|
high visibility cockpit
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gptkbp:design_philosophy
|
focus on safety and reliability
|
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gptkbp:engine
|
Rotax 912
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gptkbp:engine_type
|
four-stroke engine
|
|
gptkbp:first_flight
|
gptkb:1985
|
|
gptkbp:fuel_capacity
|
50 liters
|
|
gptkbp:fuel_type
|
MOGAS or AVGAS
|
|
gptkbp:fuselage_material
|
gptkb:NACA_4412
composite materials
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grobs G115 E Tutor
|
|
gptkbp:introduced
|
gptkb:1985
|
|
gptkbp:landing_distance
|
300 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:maintenance
|
easy maintenance access
|
|
gptkbp:manufacturer
|
gptkb:Grobs_Aircraft
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:market_segment
|
flight training market
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:notable_users
|
various flying schools
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:offers_certificate
|
gptkb:EASA
|
|
gptkbp:operational_history
|
used in various countries
|
|
gptkbp:passenger_capacity
|
gptkb:1
|
|
gptkbp:performance
|
good performance characteristics
|
|
gptkbp:production_location
|
gptkb:Germany
|
|
gptkbp:production_years
|
1985-2000
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:provides_training_for
|
aerobatics training
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:Grob_G115_family
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:safety_record
|
good safety record
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:stall_speed
|
65 km/h
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
400 m
|
|
gptkbp:training
|
basic flight training
initial pilot training
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:weight_limit
|
900 kg
|
|
gptkbp:wing_area
|
16.5 m²
|
|
gptkbp:wing_configuration
|
low-wing
cantilever wing
|
|
gptkbp:wingspan
|
14.2 m
|
|
gptkbp:bfsParent
|
gptkb:No._2_Flying_Training_School_RAF
gptkb:No._10_Flying_Training_School_RAF
gptkb:No._11_Flying_Training_School_RAF
gptkb:No._7_Flying_Training_School
|
|
gptkbp:bfsLayer
|
5
|