Zlin Z-50 M-1

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aerobatic_capabilities full aerobatic capabilities
gptkbp:aircraft_configuration single-engine
gptkbp:aircraft_operated gptkb:light_aircraft
gptkbp:aircraft_role sport aviation
gptkbp:capacity gptkb:1
gptkbp:climb_rate 5 m/s
gptkbp:cockpit open cockpit
gptkbp:controls stick control
gptkbp:country_of_origin gptkb:Czech_Republic
gptkbp:crew gptkb:1
gptkbp:cruise_speed 200 km/h
gptkbp:design aerobatics
Zlin design team
gptkbp:engine gptkb:Lycoming_IO-360
gptkbp:first_flight gptkb:1970
gptkbp:flaps split flaps
gptkbp:fuel_capacity 100 liters
gptkbp:fuselage_material gptkb:NACA_4412
monocoque construction
gptkbp:has_limitations +6/-3 g
gptkbp:height 2.3 m
gptkbp:historical_significance important in Czech aviation history
https://www.w3.org/2000/01/rdf-schema#label Zlin Z-50 M-1
gptkbp:introduced gptkb:1970
gptkbp:landing_distance 250 m
gptkbp:landing_gear tricycle gear
gptkbp:length 7.2 m
gptkbp:manufacturer gptkb:Zlin_Aircraft
gptkbp:max_takeoff_weight 800 kg
gptkbp:notable_features good maneuverability
gptkbp:number_built over 200
gptkbp:production_years 1970-1980s
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion 0.45 k W/kg
gptkbp:range 1,000 km
gptkbp:related_show popular in airshows
gptkbp:retired 2000s
gptkbp:roll_rate 360°/s
gptkbp:service_ceiling 3,000 m
gptkbp:stall_speed 65 km/h
docile stall
gptkbp:successor gptkb:Zlin_Z-142
gptkbp:tail_type conventional tail
gptkbp:takeoff_distance 300 m
gptkbp:training pilot training
gptkbp:type aerobatic aircraft
gptkbp:used_by aerobatic teams
gptkbp:variant Zlin Z-50 M, Zlin Z-50 LS
gptkbp:wing_area 12.5 m²
gptkbp:wing_configuration low-wing
64 kg/m²
gptkbp:wingspan 8.5 m
gptkbp:bfsParent gptkb:Zlin_Z-50_M
gptkbp:bfsLayer 9