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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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general aviation
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gptkbp:avionics
|
modern avionics suite
|
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gptkbp:cockpit
|
glass cockpit
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
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gptkbp:country_of_origin
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gptkb:Romania
|
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gptkbp:crew
|
2
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gptkbp:cruise_speed
|
200 km/h
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gptkbp:design
|
low-wing monoplane
IAR design team
|
|
gptkbp:engine
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gptkb:Lycoming_IO-360
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gptkbp:engine_power
|
180 hp
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gptkbp:engine_type
|
piston engine
|
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gptkbp:first_delivery
|
gptkb:2016
|
|
gptkbp:first_flight
|
gptkb:2015
|
|
gptkbp:flaps
|
manual flaps
|
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gptkbp:fuel_capacity
|
200 L
|
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gptkbp:fuel_type
|
aviation gasoline
|
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gptkbp:fuselage_material
|
composite materials
|
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gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 821
|
|
gptkbp:intended_use
|
pilot training
|
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gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
retractable landing gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:market
|
gptkb:civil_aviation
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:number_built
|
50+
|
|
gptkbp:passenger_capacity
|
2
|
|
gptkbp:payload_capacity
|
400 kg
|
|
gptkbp:production_status
|
in production
|
|
gptkbp:production_years
|
gptkb:2015
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:regulatory_compliance
|
gptkb:EASA_CS-23
|
|
gptkbp:role
|
gptkb:trainer_aircraft
aerobatic training
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:stall_speed
|
65 km/h
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:variant
|
gptkb:IAR_821_A
gptkb:IAR_821_B
gptkb:IAR_821_C
|
|
gptkbp:weight
|
750 kg
450 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wing_configuration
|
aluminum
|
|
gptkbp:wingspan
|
10.2 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_99_Soim
|
|
gptkbp:bfsLayer
|
6
|