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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
|
general aviation
|
|
gptkbp:avionics
|
basic avionics package
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:country_of_origin
|
gptkb:Romania
|
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gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
200 km/h
|
|
gptkbp:design
|
utility aircraft
IAR design team
|
|
gptkbp:design_features
|
low stall speed
|
|
gptkbp:engine
|
piston engine
|
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gptkbp:engine_type
|
four-stroke engine
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
150 L
|
|
gptkbp:fuselage_material
|
high-wing configuration
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 95 B-4
|
|
gptkbp:introduced
|
gptkb:1995
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
IAR
|
|
gptkbp:market
|
gptkb:civil_aviation
|
|
gptkbp:market_segment
|
gptkb:light_aircraft
|
|
gptkbp:max_speed
|
220 km/h
|
|
gptkbp:max_takeoff_weight
|
1200 kg
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:primary_user
|
flying schools
|
|
gptkbp:produces
|
limited production
50 units
|
|
gptkbp:production_years
|
1995-2000
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:propulsion
|
propeller-driven
|
|
gptkbp:range
|
800 km
|
|
gptkbp:regulatory_compliance
|
EASA standards
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:safety_features
|
dual controls
|
|
gptkbp:service_ceiling
|
3000 m
|
|
gptkbp:status
|
in production
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:variant
|
IAR 95 B-4 A
IAR 95 B-4 B
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:IAR_95_B
|
|
gptkbp:bfsLayer
|
8
|