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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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conventional configuration
low-cost design
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gptkbp:aircraft_operated
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general aviation
flight training
good visibility
influenced future designs
good performance
popular in Poland
part of Polish aviation history
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gptkbp:aircraft_role
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gptkb:trainer_aircraft
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:controls
|
yoke
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gptkbp:country_of_origin
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gptkb:Poland
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gptkbp:crew
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gptkb:1
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gptkbp:cruise_speed
|
200 km/h
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gptkbp:design
|
gptkb:Mieczysław_Kocjan
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gptkbp:engine
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gptkb:Lycoming_O-360
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gptkbp:engine_type
|
piston engine
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gptkbp:first_flight
|
gptkb:1986
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gptkbp:flaps
|
manual flaps
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gptkbp:fuel_capacity
|
120 L
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gptkbp:fuselage_material
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gptkb:metal
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gptkbp:height
|
2.5 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
PZL-110 Koliber
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
8.0 m
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gptkbp:manufacturer
|
PZL
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gptkbp:marketed_as
|
gptkb:PZL-110_Koliber
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gptkbp:max_takeoff_weight
|
1,200 kg
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gptkbp:number_built
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50
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gptkbp:offers_certificate
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gptkb:EASA
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gptkbp:passenger_capacity
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gptkb:3
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gptkbp:production_location
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gptkb:Poland
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gptkbp:production_years
|
1986-1990
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gptkbp:propeller
|
variable-pitch propeller
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gptkbp:range
|
1,200 km
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gptkbp:role
|
utility aircraft
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gptkbp:service_ceiling
|
3,000 m
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gptkbp:stall_speed
|
65 km/h
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gptkbp:successor
|
PZL-120
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gptkbp:tail_type
|
T-tail
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gptkbp:type
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gptkb:light_aircraft
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gptkbp:variant
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PZL-110 Koliber 2
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gptkbp:wing_area
|
15 m²
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gptkbp:wing_configuration
|
high-wing
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gptkbp:wingspan
|
10.5 m
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gptkbp:bfsParent
|
gptkb:PZL-130_Orlik
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gptkbp:bfsLayer
|
6
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