Zlin Z-39

URI: https://gptkb.org/entity/Zlin_Z-39
GPTKB entity
Statements (45)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 8
gptkbp:bfsParent gptkb:Zlin_Z-526_M
gptkbp:aspect_ratio 7.0
gptkbp:climb_rate 5 m/s
gptkbp:cockpit open cockpit
gptkbp:crew gptkb:musical
gptkbp:design gptkb:Zlin_Aircraft_Company
gptkbp:engine gptkb:Avia_M-137
gptkbp:first_flight gptkb:1960
gptkbp:flaps split flaps
gptkbp:fuel_capacity 120 L
gptkbp:height 2.4 m
gptkbp:historical_significance popular trainer in Eastern Europe.
https://www.w3.org/2000/01/rdf-schema#label Zlin Z-39
gptkbp:introduced gptkb:1960
gptkbp:is_used_by gptkb:Czech_Air_Force
gptkbp:landing_gear tricycle gear
gptkbp:length 8.2 m
gptkbp:manufacturer gptkb:Zlin_Aircraft
gptkbp:material gptkb:NACA_2412
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 300 m
400 m
1,200 kg
gptkbp:notable_features good visibility
gptkbp:number_built over 200
gptkbp:power_output 140 hp
gptkbp:primary_user flight schools
gptkbp:production_years 1960-1970s
gptkbp:propulsion two-bladed
gptkbp:range 800 km
gptkbp:retired 1990s
gptkbp:role gptkb:aircraft
gptkbp:roll_rate 3.5°/s
gptkbp:service_ceiling 4,000 m
gptkbp:setting low-wing monoplane
gptkbp:speed 65 km/h
gptkbp:successor gptkb:Zlin_Z-142
gptkbp:surface elevator, ailerons, rudder
gptkbp:tail_type conventional tail
gptkbp:type single-engine
gptkbp:variant Zlin Z-39 M
gptkbp:wing_area 14.5 m²
gptkbp:wingspan 10.5 m