|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Zlin_Aviation
|
|
gptkbp:aircraft_operated
|
gptkb:item
general aviation
aerobatic training
private flying
aerial work
glider towing
|
|
gptkbp:aspect_ratio
|
6.5
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:controls
|
conventional control surfaces
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
Miloš Šťastný
|
|
gptkbp:engine
|
gptkb:Avia_M-137_A
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
100 L
|
|
gptkbp:height
|
2.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-526 X
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_takeoff_weight
|
200 m
250 m
950 kg
|
|
gptkbp:notable_users
|
gptkb:Czech_Air_Force
various flying clubs
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:power_output
|
140 hp
|
|
gptkbp:production_years
|
1965-1970
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
1-3
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:setting
|
low-wing monoplane
|
|
gptkbp:speed
|
65 km/h
200 km/h
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
gptkb:Zlin_Z-526_A
gptkb:Zlin_Z-526_F
gptkb:Zlin_Z-526_L
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wingspan
|
9.5 m
|