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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:avionics
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basic instrumentation
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gptkbp:climb_rate
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3.5 m/s
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gptkbp:cockpit
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tandem seating
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gptkbp:community
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active owner community
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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:cruise_speed
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160 km/h
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gptkbp:design
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gptkb:Burkhard_Grob
general aviation
low-wing monoplane
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gptkbp:design_feature
|
easy handling
good visibility
robust construction
low drag design
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gptkbp:engine_power
|
100 hp
|
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gptkbp:engine_type
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piston engine
|
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gptkbp:financial_stability
|
high stability
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gptkbp:first_flight
|
gptkb:1980
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gptkbp:flaps
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gptkb:manual
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gptkbp:fuel_capacity
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100 L
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Grobs G115 E
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gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
popular trainer aircraft
|
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gptkbp:length
|
8.2 m
|
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gptkbp:maintenance
|
easy maintenance
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gptkbp:manufacturer
|
Grobs
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gptkbp:market
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gptkb:civil_aviation
|
|
gptkbp:market_segment
|
entry-level aircraft
|
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gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_users
|
various flight schools
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|
gptkbp:number_built
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over 1,000
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|
gptkbp:offers_certificate
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gptkb:EASA
|
|
gptkbp:operational_cost
|
low operational cost
|
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gptkbp:passenger_capacity
|
2
|
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gptkbp:performance
|
good maneuverability
|
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gptkbp:production_years
|
1980-1990
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gptkbp:propeller
|
variable pitch
|
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gptkbp:range
|
1,000 km
|
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gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:safety_record
|
generally safe
|
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gptkbp:service_ceiling
|
4,500 m
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|
gptkbp:stall_speed
|
60 km/h
|
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gptkbp:support
|
manufacturer support
|
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gptkbp:tail_type
|
T-tail configuration
|
|
gptkbp:training
|
pilot training
aerobatic training
|
|
gptkbp:variant
|
G115 A
G115 B
G115 C
G115 D
|
|
gptkbp:weight
|
600 kg
|
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gptkbp:wing_area
|
20 m²
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|
gptkbp:wingspan
|
15.2 m
|
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gptkbp:bfsParent
|
gptkb:RAF_Shawbury
gptkb:No._12_Flying_Training_School_RAF
gptkb:No._7_Flying_Training_School_RAF
gptkb:No._1_Flying_Training_School
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gptkbp:bfsLayer
|
5
|