Zlin Z-526 D

URI: https://gptkb.org/entity/Zlin_Z-526_D
GPTKB entity
Statements (47)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 7
gptkbp:bfsParent gptkb:Zlin_Aviation
gptkbp:aircraft_operated general aviation
single-engine
low-wing
gptkbp:cockpit two-seat tandem
gptkbp:controls dual control
gptkbp:crew gptkb:musical
gptkbp:design Václav Krištof
gptkbp:engine gptkb:Avia_M137
gptkbp:first_flight gptkb:1965
gptkbp:flaps split flaps
gptkbp:fuel_capacity 120 L
gptkbp:height 2.4 m
https://www.w3.org/2000/01/rdf-schema#label Zlin Z-526 D
gptkbp:is_used_for gptkb:battle
gptkbp:landing_gear tricycle gear
gptkbp:length 8.2 m
gptkbp:manufacturer gptkb:Zlin_Aircraft
gptkbp:market gptkb:Europe
gptkbp:material gptkb:NACA_4412
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 200 m
250 m
950 kg
gptkbp:members 2.5°/s
gptkbp:notable_users gptkb:Czech_Air_Force
gptkbp:number_built over 1000
gptkbp:operational_history used by flying clubs
gptkbp:origin gptkb:Monarch
gptkbp:production_years 1965-1975
gptkbp:propulsion two-bladed
gptkbp:range 800 km
gptkbp:role aerobatic training
gptkbp:roll_rate 3.5°/s
gptkbp:seating_capacity 1-3
gptkbp:service_ceiling 4000 m
gptkbp:speed 65 km/h
gentle stall
gptkbp:strikeouts 4.0°/s
gptkbp:successor gptkb:Zlin_Z-142
gptkbp:type gptkb:aircraft
gptkbp:variant gptkb:Zlin_Z-526_F
gptkbp:weight 600 kg
gptkbp:wing_area 14.5 m²
gptkbp:wingspan 10.5 m