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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Pipistrel_Sinus
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
cantilever wing
|
|
gptkbp:category
|
ultralight aircraft
|
|
gptkbp:climb_rate
|
3.5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:controls
|
stick control
|
|
gptkbp:design
|
aerodynamic efficiency
high-wing
|
|
gptkbp:engine
|
gptkb:Rotax_912_ULS
|
|
gptkbp:engine_type
|
four-stroke engine
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:first_flight
|
gptkb:2003
stable flight
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
50 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pipistrel Sinus 912 ULS
|
|
gptkbp:inspiration
|
gliders
|
|
gptkbp:instrument
|
gptkb:GPS
gptkb:radio_station
|
|
gptkbp:interior_features
|
two-seat configuration
|
|
gptkbp:landing_gear
|
tricycle gear
fixed landing gear
|
|
gptkbp:manufacturer
|
gptkb:Pipistrel
|
|
gptkbp:market_segment
|
recreational flying
|
|
gptkbp:marketed_as
|
flight training
affordable aircraft
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
600 kg
|
|
gptkbp:notable_feature
|
glider-like performance
|
|
gptkbp:operational_area
|
low operational cost
|
|
gptkbp:origin
|
gptkb:Slovenia
|
|
gptkbp:performance
|
excellent climb performance
|
|
gptkbp:production_years
|
2003-present
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:regulatory_compliance
|
EASA certified
FAR 23
|
|
gptkbp:safety_features
|
crash-resistant fuel system
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service_ceiling
|
3,000 meters
|
|
gptkbp:speed
|
160 km/h
60 km/h
|
|
gptkbp:surface
|
gptkb:public_transportation_system
rudder
aileron
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
used for flight schools
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:user_base
|
private pilots
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:wing_area
|
monocoque
15.5 m²
|
|
gptkbp:wingspan
|
10.7 meters
|