IAR 358 A

GPTKB entity

Predicate	Object
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:avionics	basic avionics
gptkbp:climb_rate	5 m/s
gptkbp:cockpit	tandem seating
gptkbp:cockpit_instruments	analog instruments
gptkbp:crew	2
gptkbp:design	low-wing monoplane IAR design team
gptkbp:engine_power	180 hp
gptkbp:engine_type	piston engine
gptkbp:first_delivery	gptkb:1981
gptkbp:first_flight	gptkb:1980 1990s
gptkbp:fuel_capacity	200 L
gptkbp:height	2.80 m
https://www.w3.org/2000/01/rdf-schema#label	IAR 358 A
gptkbp:introduced	gptkb:1980
gptkbp:landing_distance	300 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	50
gptkbp:offers_certificate	obtained
gptkbp:primary_user	gptkb:Romanian_Air_Force
gptkbp:production_years	1980-1985
gptkbp:propeller	two-bladed
gptkbp:range	1,000 km
gptkbp:role	gptkb:trainer_aircraft
gptkbp:rollout_distance	200 m
gptkbp:service_ceiling	4,500 m
gptkbp:stall_speed	70 km/h
gptkbp:successor	gptkb:IAR_99
gptkbp:takeoff_distance	400 m
gptkbp:training	pilot training
gptkbp:variant	gptkb:IAR_358_B
gptkbp:wing_area	12.5 m²
gptkbp:wingspan	9.50 m
gptkbp:bfsParent	gptkb:IAR_358
gptkbp:bfsLayer	8