|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
general aviation
800 kg
|
|
gptkbp:aircraft_role
|
primary trainer
|
|
gptkbp:aircraft_type
|
civil aircraft
|
|
gptkbp:avionics
|
basic instrumentation
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:competitors
|
gptkb:Cessna_152
|
|
gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:Germany
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:cruise_speed
|
120 knots
|
|
gptkbp:design
|
gptkb:Burkhard_Grob
|
|
gptkbp:design_date
|
gptkb:1978
|
|
gptkbp:design_features
|
low stall speed
|
|
gptkbp:design_purpose
|
flight training
|
|
gptkbp:emergency_services
|
gptkb:parachute
|
|
gptkbp:engine
|
gptkb:Lycoming
|
|
gptkbp:engine_configuration
|
nose-mounted
|
|
gptkbp:engine_power
|
100 hp
|
|
gptkbp:engine_type
|
piston engine
O-235
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
100 liters
|
|
gptkbp:fuselage_material
|
composite materials
high-wing configuration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob Tutor IIe-2000
|
|
gptkbp:interior_features
|
dual controls
|
|
gptkbp:landing_distance
|
65 knots
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 meters
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:market_launch
|
gptkb:1980
|
|
gptkbp:market_segment
|
gptkb:trainer_aircraft
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_users
|
flight schools
|
|
gptkbp:offers_certificate
|
gptkb:EASA
|
|
gptkbp:passenger_capacity
|
1 passenger
|
|
gptkbp:power_consumption
|
12 kg/hp
|
|
gptkbp:production_status
|
out of production
|
|
gptkbp:production_years
|
1980-1990
|
|
gptkbp:propeller
|
fixed-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:service_ceiling
|
4,000 meters
|
|
gptkbp:service_history
|
used in various flight schools
|
|
gptkbp:squadrons
|
white and blue
|
|
gptkbp:stall_speed
|
60 knots
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:transportation
|
20 knots
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wing_configuration
|
cantilever wing
77 kg/m²
|
|
gptkbp:wingspan
|
11.5 meters
|
|
gptkbp:bfsParent
|
gptkb:Grob_Tutor_II
|
|
gptkbp:bfsLayer
|
8
|