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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
7:1
|
|
gptkbp:certification
|
Yugoslav certification
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:controls
|
frise ailerons
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
1 × piston engine
|
|
gptkbp:first_flight
|
gptkb:1975
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
conventional
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
UTVA-75
|
|
gptkbp:introduced
|
gptkb:1975
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:UTVA
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
good visibility from cockpit
|
|
gptkbp:notable_ships
|
balanced rudder
|
|
gptkbp:number_built
|
over 100
|
|
gptkbp:operational_history
|
used for training and aerobatics
|
|
gptkbp:primary_user
|
gptkb:Yugoslav_Air_Force
|
|
gptkbp:production_years
|
1975-1990
|
|
gptkbp:range
|
800 km
|
|
gptkbp:related_aircraft
|
gptkb:UTVA-66
gptkb:Soko_J-20_Kraguj
gptkb:Soko_G-2_Galeb
UTVA-75 A
UTVA-75 B
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
UTVA-75 A
|
|
gptkbp:tailplane_material
|
gptkb:metal
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:variant
|
UTVA-75 A
UTVA-75 B
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wing_configuration
|
gptkb:metal
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:UTVA
|
|
gptkbp:bfsLayer
|
7
|