gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:armament
|
gptkb:none
|
gptkbp:aspect_ratio
|
7.0
|
gptkbp:certification
|
gptkb:none
yes
|
gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
gptkbp:crew
|
2
|
gptkbp:design
|
low-wing monoplane
|
gptkbp:engine_power
|
180 hp
|
gptkbp:engine_type
|
piston engine
|
gptkbp:first_flight
|
gptkb:1980
|
gptkbp:flaps
|
split flaps
|
gptkbp:fuel_capacity
|
200 liters
|
gptkbp:fuselage_material
|
gptkb:metal
gptkb:NACA_2412
|
gptkbp:has_museum
|
yes
|
gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
UTVA-90
|
gptkbp:introduced
|
gptkb:1980
|
gptkbp:landing_distance
|
400 m
|
gptkbp:landing_gear
|
tricycle 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_case
|
none reported
|
gptkbp:notable_pilots
|
yes
|
gptkbp:number_built
|
over 100
|
gptkbp:operational_history
|
used in the 1980s and 1990s
|
gptkbp:primary_user
|
gptkb:Yugoslav_Air_Force
|
gptkbp:production_years
|
1980-1990
|
gptkbp:propeller
|
two-bladed
|
gptkbp:range
|
1,000 km
|
gptkbp:related_aircraft
|
gptkb:UTVA-75
|
gptkbp:related_show
|
yes
|
gptkbp:retired
|
2000s
|
gptkbp:role
|
gptkb:trainer_aircraft
|
gptkbp:roll_rate
|
3.0°/s
|
gptkbp:service_ceiling
|
4,500 m
|
gptkbp:stall_speed
|
70 km/h
12°
|
gptkbp:successor
|
gptkb:none
|
gptkbp:tail_type
|
T-tail
|
gptkbp:takeoff_distance
|
300 m
|
gptkbp:training
|
basic flight training
|
gptkbp:variant
|
gptkb:UTVA-75
|
gptkbp:weight
|
400 kg
800 kg
|
gptkbp:wing_area
|
15 m²
|
gptkbp:wing_configuration
|
gptkb:metal
|
gptkbp:wingspan
|
10.5 m
|
gptkbp:bfsParent
|
gptkb:UTVA
|
gptkbp:bfsLayer
|
7
|