Zlin Z-42

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:capacity 2
gptkbp:cockpit two-seat tandem
gptkbp:controls conventional control surfaces
gptkbp:country_of_origin gptkb:Czechoslovakia
gptkbp:crew gptkb:1
gptkbp:design gptkb:Zlin_Aircraft_Company
gptkbp:engine gptkb:Avia_M137
gptkbp:first_flight gptkb:1968
gptkbp:flaps split flaps
gptkbp:fuel_capacity 120 liters
gptkbp:fuselage_material gptkb:NACA_2412
monocoque construction
gptkbp:height 2.40 m
https://www.w3.org/2000/01/rdf-schema#label Zlin Z-42
gptkbp:landing_distance 400 m
gptkbp:landing_gear tricycle gear
gptkbp:length 8.20 m
gptkbp:manufacturer gptkb:Zlin_Aircraft
gptkbp:marketed_as gptkb:Zlin_Z-42_trainer
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 1,200 kg
gptkbp:notable_features durable construction
easy handling
low operating costs
good visibility
good climb rate
stable flight characteristics
low stall speed
gptkbp:number_built over 200
gptkbp:power_output 140 hp
gptkbp:production_years 1968-1980
gptkbp:propeller two-bladed
gptkbp:range 1,000 km
gptkbp:related_aircraft gptkb:Zlin_Z-43
gptkb:Zlin_Z-50
gptkbp:role gptkb:trainer_aircraft
gptkbp:service_ceiling 4,000 m
gptkbp:stall_speed 65 km/h
gptkbp:tail_type T-tail configuration
gptkbp:takeoff_distance 300 m
gptkbp:type gptkb:light_aircraft
gptkbp:used_by various flying schools
gptkbp:variant Z-42 C
Z-42 L
Z-42 M
gptkbp:wing_area 14.5 m²
gptkbp:wing_configuration high-wing
gptkbp:wingspan 10.80 m
gptkbp:bfsParent gptkb:Letov_Š-328_A
gptkb:Zlin_Aircraft
gptkb:Zlin_Aircraft_Company
gptkbp:bfsLayer 7