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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
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gptkbp:bfsParent
|
gptkb:Zlin_Aviation
|
|
gptkbp:aircraft_operated
|
Piper PA-28
light aircraft category
|
|
gptkbp:avionics
|
basic avionics
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:controls
|
yoke
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
gptkb:aircraft
Zlin design team
|
|
gptkbp:engine
|
gptkb:Lycoming_O-360
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
low-wing design
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
120 liters
|
|
gptkbp:height
|
2.4 m
|
|
gptkbp:historical_significance
|
popular trainer aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Zlin Z-526 W
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
gptkb:Zlin_Aircraft
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:market_segment
|
gptkb:aircraft
|
|
gptkbp:material
|
gptkb:NACA_4412
monocoque construction
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
70 km/h
1,200 kg
|
|
gptkbp:notable_users
|
gptkb:Czech_Air_Force
|
|
gptkbp:number_built
|
over 500
|
|
gptkbp:operational_area
|
gptkb:aircraft
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:performance
|
good performance
|
|
gptkbp:production_location
|
gptkb:Zlin,_Czech_Republic
|
|
gptkbp:production_years
|
1965-1975
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:safety_record
|
good safety record
|
|
gptkbp:seating_capacity
|
gptkb:3
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:surface
|
elevator and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Z-526 F
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|