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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
single-engine aircraft
high-wing
light sport aircraft
77 kg/m²
|
|
gptkbp:avionics
|
modern avionics system
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:constructionMaterial
|
metal construction
semi-monocoque fuselage
|
|
gptkbp:countryOfOrigin
|
gptkb:Poland
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
low stall speed
Witold S. Kwiatkowski
versatile training aircraft
|
|
gptkbp:engine
|
Lycoming O-360
|
|
gptkbp:engineType
|
four-cylinder engine
|
|
gptkbp:firstFlight
|
1990
|
|
gptkbp:fuelCapacity
|
150 L
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PZL-110 Koliber
|
|
gptkbp:introduced
|
1991
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.0 m
|
|
gptkbp:manufacturer
|
PZL
|
|
gptkbp:marketedAs
|
flight training schools
training and recreational aircraft
|
|
gptkbp:marketSegment
|
general aviation
|
|
gptkbp:maxSpeed
|
220 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notableUsers
|
gptkb:Polish_Air_Force
|
|
gptkbp:numberBuilt
|
over 100
|
|
gptkbp:operationalHistory
|
used in flight schools
|
|
gptkbp:passengerCapacity
|
3
|
|
gptkbp:performance
|
good performance for training
|
|
gptkbp:powerOutput
|
6.0 kg/hp
|
|
gptkbp:productionCompany
|
1991-2000
|
|
gptkbp:productionLocation
|
gptkb:Poland
|
|
gptkbp:products
|
EASA_type_certificate
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:regulatoryCompliance
|
EASA_standards
|
|
gptkbp:relatedAircraft
|
gptkb:PZL-104_Wilga
|
|
gptkbp:retired
|
still in service
|
|
gptkbp:revenue
|
1991
|
|
gptkbp:role
|
training aircraft
|
|
gptkbp:safetyFeatures
|
parachute recovery system
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:speed
|
65 km/h
200 km/h
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
light aircraft
|
|
gptkbp:variant
|
PZL-110 Koliber 2
|
|
gptkbp:weight
|
750 kg
|
|
gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|