|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
gptkb:Burkhard_Grob
|
|
gptkbp:design_purpose
|
basic flight training
advanced flight training
aerobatics training
|
|
gptkbp:engine_power
|
100 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:flaps
|
gptkb:manual
|
|
gptkbp:fuel_capacity
|
50 liters
|
|
gptkbp:fuselage_material
|
composite
high-wing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob Tutor IIe-2200
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:market
|
gptkb:civil_aviation
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:notable_users
|
gptkb:Royal_Air_Force
gptkb:Austrian_Air_Force
gptkb:Luftwaffe
gptkb:Swiss_Air_Force
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:offers_certificate
|
gptkb:EASA
|
|
gptkbp:operational_history
|
used by flying schools
|
|
gptkbp:passenger_capacity
|
1 passenger
|
|
gptkbp:performance
|
good maneuverability
|
|
gptkbp:production_years
|
1980-1990
|
|
gptkbp:propeller
|
fixed-pitch
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:stall_speed
|
60 km/h
|
|
gptkbp:trademark
|
Grob
|
|
gptkbp:training
|
flight training
|
|
gptkbp:variant
|
Grob Tutor IIe-2200 B
Grob Tutor IIe-2200 C
Grob Tutor IIe-2200 D
Grob Tutor IIe-2200 E
|
|
gptkbp:weight
|
500 kg
|
|
gptkbp:weight_limit
|
800 kg
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:Grob_Tutor_II
|
|
gptkbp:bfsLayer
|
8
|