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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_traffic_control
|
manual controls
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:aircraft_role
|
gptkb:civil_aviation
|
|
gptkbp:aircraft_type
|
fixed-wing aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:IAR_358
IAR design team
|
|
gptkbp:design_purpose
|
training and leisure flying
|
|
gptkbp:emergency_services
|
gptkb:parachute
|
|
gptkbp:engine_power
|
180 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
gptkbp:height
|
2.80 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 358 B
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
low-wing monoplane
|
|
gptkbp:number_built
|
50
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:offers_certificate
|
obtained
|
|
gptkbp:operational_history
|
used for training
|
|
gptkbp:primary_user
|
gptkb:Romanian_Air_Force
|
|
gptkbp:production_location
|
gptkb:Romania
|
|
gptkbp:production_years
|
1980-1990
|
|
gptkbp:propeller
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
gptkb:light_aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:variant
|
gptkb:IAR_358_A
gptkb:IAR_358_C
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wing_configuration
|
high-wing
|
|
gptkbp:wingspan
|
9.50 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_358
|
|
gptkbp:bfsLayer
|
8
|