|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aspect_ratio
|
7.0
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:combat_role
|
pilot training
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:IAR_823_engine
|
|
gptkbp:engine_power
|
180 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1960
gptkb:1970
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuselage_material
|
gptkb:metal
gptkb:NACA_4412
|
|
gptkbp:height
|
2.80 m
|
|
gptkbp:historical_significance
|
used in Romanian military training
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 823
|
|
gptkbp:introduced
|
gptkb:1960
gptkb:1970
|
|
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:number_built
|
gptkb:100
50
|
|
gptkbp:payload_capacity
|
400 kg
|
|
gptkbp:primary_user
|
gptkb:Romanian_Air_Force
|
|
gptkbp:production_location
|
gptkb:Romania
|
|
gptkbp:production_years
|
gptkb:1960
gptkb:1965
|
|
gptkbp:propeller
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:IAR_826
IAR 814
|
|
gptkbp:retired
|
gptkb:1980s
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:IAR_826
gptkb:IAR_99
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:variant
|
IAR 823 A
IAR 823 B
IAR 823 C
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wing_configuration
|
gptkb:metal
|
|
gptkbp:wingspan
|
10.50 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_99
gptkb:IAR_Brașov
|
|
gptkbp:bfsLayer
|
7
|