Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:aircraft_operated |
gptkb:light_aircraft
|
| gptkbp:cockpit |
open cockpit
|
| gptkbp:crew |
1 pilot
|
| gptkbp:design |
basic trainer
|
| gptkbp:engine_type |
piston engine
|
| gptkbp:first_flight |
gptkb:1975
|
| gptkbp:fuel_capacity |
150 L
|
| https://www.w3.org/2000/01/rdf-schema#label |
UTVA 75 B
|
| 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:number_built |
50
|
| gptkbp:number_of_engines |
gptkb:1
|
| gptkbp:offers_certificate |
gptkb:Yugoslavia
|
| gptkbp:primary_user |
gptkb:Yugoslav_Air_Force
|
| gptkbp:production_years |
1975-1980
|
| gptkbp:propeller |
two-bladed propeller
|
| gptkbp:related_aircraft |
gptkb:Cessna_152
|
| gptkbp:role |
gptkb:trainer_aircraft
civilian training |
| gptkbp:service_ceiling |
4,500 m
|
| gptkbp:variant |
gptkb:UTVA_75_B-1
gptkb:UTVA_75_B-2 |
| gptkbp:weight |
800 kg
|
| gptkbp:wingspan |
10.5 m
|
| gptkbp:bfsParent |
gptkb:UTVA_75
|
| gptkbp:bfsLayer |
6
|