gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
gptkbp:armament
|
gptkb:none
|
gptkbp:certification
|
yes
|
gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:country_of_origin
|
gptkb:Romania
|
gptkbp:crew
|
2
|
gptkbp:design
|
basic trainer
IAR design team
|
gptkbp:engine_power
|
180 hp
|
gptkbp:engine_type
|
piston engine
|
gptkbp:first_flight
|
gptkb:1958
1958-06-01
|
gptkbp:fuel_capacity
|
200 L
|
gptkbp:height
|
2.80 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 181
|
gptkbp:intended_use
|
pilot training
|
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:nickname
|
none known
|
gptkbp:number_built
|
approximately 200
|
gptkbp:operational_history
|
used by Romanian Air Force
|
gptkbp:payload_capacity
|
400 kg
|
gptkbp:power_source
|
IAR 14
|
gptkbp:production_location
|
gptkb:Romania
|
gptkbp:production_years
|
1958-1965
|
gptkbp:propeller
|
two-bladed propeller
|
gptkbp:range
|
1,000 km
|
gptkbp:related_aircraft
|
IAR 813
|
gptkbp:retired
|
1990s
|
gptkbp:role
|
gptkb:trainer_aircraft
|
gptkbp:service_ceiling
|
4,500 m
|
gptkbp:stall_speed
|
70 km/h
|
gptkbp:successor
|
gptkb:IAR_823
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:takeoff_distance
|
300 m
|
gptkbp:variant
|
IAR 181 S
|
gptkbp:wing_area
|
15.5 m²
|
gptkbp:wing_configuration
|
high-wing
|
gptkbp:wingspan
|
10.50 m
|
gptkbp:bfsParent
|
gptkb:IAR_180
|
gptkbp:bfsLayer
|
9
|