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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:Romania
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
IAR design team
|
|
gptkbp:design_features
|
high-wing configuration
|
|
gptkbp:design_philosophy
|
simplicity and reliability
|
|
gptkbp:engine
|
gptkb:Lycoming_O-320
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:exhibits
|
aviation museums
|
|
gptkbp:first_flight
|
gptkb:1970
1970-06-15
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
100 L
|
|
gptkbp:fuselage_material
|
gptkb:NACA_2412
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_significance
|
used for pilot training
contributed to aviation in Romania
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 111-3
|
|
gptkbp:influences
|
subsequent IAR designs
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
foundation for future IAR aircraft.
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:market
|
gptkb:civil_aviation
gptkb:military_training
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
750 kg
|
|
gptkbp:notable_users
|
gptkb:Romanian_Air_Force
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:passenger_capacity
|
2
|
|
gptkbp:performance
|
short takeoff and landing
good climb rate
stable flight characteristics
|
|
gptkbp:production_years
|
1970-1980
|
|
gptkbp:propeller
|
fixed-pitch propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:related_model
|
gptkb:IAR_111-4
gptkb:IAR_111-2
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:trademark
|
IAR
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_111_series
|
|
gptkbp:bfsLayer
|
8
|