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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:air_support
|
certified
|
|
gptkbp:air_traffic_control
|
yoke
|
|
gptkbp:availability
|
in production
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:construction_material
|
composite materials
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:country_of_origin
|
gptkb:Romania
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
200 km/h
|
|
gptkbp:design
|
utility aircraft
IAR design team
|
|
gptkbp:design_date
|
gptkb:2010
|
|
gptkbp:design_philosophy
|
ease of handling
|
|
gptkbp:engine
|
gptkb:Lycoming_IO-360
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:2015
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 821 A
|
|
gptkbp:intended_use
|
training and leisure flying
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:marketed_as
|
gptkb:IAR_821_A
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:navigation_system
|
GPS, VHF radio
|
|
gptkbp:notable_features
|
high visibility cockpit
|
|
gptkbp:number_built
|
50+
|
|
gptkbp:offers_certificate
|
gptkb:EASA_CS-23
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:performance_style
|
gptkb:light_aircraft
|
|
gptkbp:production_years
|
gptkb:2015
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:propulsion
|
propeller-driven
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:safety
|
gptkb:parachute
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:stall_speed
|
65 km/h
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:target_market
|
flying schools, private owners
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.8 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_821
|
|
gptkbp:bfsLayer
|
7
|