|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
7.6
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:Romania
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
IAR team
|
|
gptkbp:design_purpose
|
basic flight training
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:financial_stability
|
high stability
|
|
gptkbp:first_flight
|
gptkb:1969
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.60 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 111 B
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:performance
|
good maneuverability
|
|
gptkbp:power_output
|
180 hp
|
|
gptkbp:primary_user
|
gptkb:Romanian_Air_Force
|
|
gptkbp:production_location
|
gptkb:Romania
|
|
gptkbp:production_years
|
1969-1975
|
|
gptkbp:propeller
|
fixed-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:IAR_316_B
gptkb:IAR_823
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:successor
|
IAR 111 B-2
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:variant
|
IAR 111 B-1
IAR 111 B-2
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wing_configuration
|
low-wing
|
|
gptkbp:wingspan
|
9.50 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_111
|
|
gptkbp:bfsLayer
|
9
|