gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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single-engine
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gptkbp:aircraft_operated
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gptkb:light_aircraft
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gptkbp:avionics
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basic navigation instruments
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gptkbp:climb_rate
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5 m/s
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gptkbp:cockpit
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tandem seating
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gptkbp:control_surfaces
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elevator, ailerons, rudder
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gptkbp:country_of_origin
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gptkb:Yugoslavia
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gptkbp:crew
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2
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gptkbp:design
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gptkb:Milan_Jovanović
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gptkbp:design_features
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low-wing monoplane
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gptkbp:design_purpose
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pilot training
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gptkbp:engine
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gptkb:Lycoming_O-360
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gptkbp:first_flight
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gptkb:1975
1975-06-01
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gptkbp:flaps
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split flaps
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gptkbp:fuel_capacity
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120 L
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gptkbp:fuselage_material
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gptkb:metal
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gptkbp:height
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2.5 m
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https://www.w3.org/2000/01/rdf-schema#label
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UTVA 75 A
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gptkbp:influences
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gptkb:Cessna_150
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gptkbp:landing_distance
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400 m
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
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8.2 m
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gptkbp:manufacturer
|
gptkb:UTVA
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gptkbp:market
|
civil aviation and military training
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gptkbp:max_speed
|
250 km/h
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gptkbp:max_takeoff_weight
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1,200 kg
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gptkbp:notable_case
|
none reported
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gptkbp:number_built
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100+
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gptkbp:operational_history
|
used in flight schools
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gptkbp:payload_capacity
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550 kg
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gptkbp:powers
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180 hp
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gptkbp:primary_user
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gptkb:Yugoslav_Air_Force
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gptkbp:production_location
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gptkb:Utva,_Serbia
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gptkbp:production_years
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1975-1985
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gptkbp:propeller
|
constant speed propeller
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gptkbp:range
|
800 km
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gptkbp:related_aircraft
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gptkb:Boeing_707
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gptkbp:retirement
|
gptkb:1985
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gptkbp:role
|
civil and military training
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gptkbp:roll_rate
|
3.5°/s
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gptkbp:service_ceiling
|
4,500 m
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gptkbp:service_entry
|
gptkb:1975
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gptkbp:stall_speed
|
65 km/h
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gptkbp:status
|
in production
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gptkbp:tail_type
|
T-tail
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gptkbp:takeoff_distance
|
300 m
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gptkbp:type
|
gptkb:trainer_aircraft
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gptkbp:variant
|
gptkb:UTVA_75_B
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gptkbp:weight
|
650 kg
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gptkbp:wing_area
|
15.5 m²
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gptkbp:wing_configuration
|
straight wing
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gptkbp:wingspan
|
10.5 m
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gptkbp:bfsParent
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gptkb:UTVA_75
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gptkbp:bfsLayer
|
6
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