UTVA 75 B-1

URI: https://gptkb.org/entity/UTVA_75_B-1
GPTKB entity
Statements (59)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_operated gptkb:light_aircraft
gptkbp:aircraft_role gptkb:training
gptkbp:armament gptkb:none
gptkbp:cockpit tandem seating
gptkbp:configuration low-wing monoplane
gptkbp:control_system conventional controls
gptkbp:country_of_origin gptkb:Yugoslavia
gptkbp:crew 2
gptkbp:design basic trainer
gptkbp:designated_as gptkb:UTVA_75_B-1
gptkbp:engine_configuration horizontally opposed
gptkbp:engine_power 180 hp
gptkbp:engine_type piston engine
gptkbp:first_flight gptkb:1975
gptkbp:first_introduced gptkb:1975
gptkbp:flaps split flaps
gptkbp:floors all-moving tailplane
gptkbp:fuel_capacity 200 L
gptkbp:fuselage_material monocoque construction
gptkbp:has_limitations +4/-2 g
gptkbp:height 2.5 m
https://www.w3.org/2000/01/rdf-schema#label UTVA 75 B-1
gptkbp:introduced_in gptkb:1975
gptkbp:landing_distance 250 m
gptkbp:landing_gear tricycle gear
retractable landing gear
gptkbp:length 8.2 m
gptkbp:manufacturer gptkb:UTVA
gptkbp:max_speed 250 km/h
gptkbp:max_takeoff_weight 1,200 kg
gptkbp:notable_ships conventional rudder
gptkbp:number_built 50
gptkbp:number_of_engines gptkb:1
gptkbp:payload_capacity 400 kg
gptkbp:power_source gptkb:Lycoming_O-360
gptkbp:primary_user gptkb:Yugoslav_Air_Force
gptkbp:production_years 1975-1980
gptkbp:propeller constant speed propeller
gptkbp:propulsion 0.25 k W/kg
gptkbp:range 800 km
gptkbp:related_aircraft gptkb:UTVA_75
gptkbp:retired gptkb:Yugoslav_Air_Force
gptkbp:role gptkb:military_training
gptkbp:roll_rate 3°/s
gptkbp:service_ceiling 4,500 m
gptkbp:stall_speed 70 km/h
gptkbp:successor gptkb:UTVA_75_B-2
gptkbp:takeoff_distance 300 m
gptkbp:type gptkb:trainer_aircraft
gptkbp:used_by gptkb:Yugoslav_Air_Force
gptkbp:variant gptkb:UTVA_75
gptkbp:weight 800 kg
gptkbp:wing_area 12.5 m²
gptkbp:wing_configuration cantilever wing
96 kg/m²
gptkbp:wingspan 10.5 m
gptkbp:bfsParent gptkb:UTVA_75_B
gptkbp:bfsLayer 7