|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aspect_ratio
|
7.0
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:country_of_origin
|
gptkb:Poland
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
high-wing monoplane
|
|
gptkbp:engine
|
gptkb:PZL-104_Wilga_80
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1962
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.60 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PZL-104 Wilga 80
|
|
gptkbp:landing_distance
|
250 m
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
PZL
|
|
gptkbp:marketed_as
|
gptkb:aircraft
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_users
|
gptkb:civil_aviation
gptkb:Polish_Air_Force
search and rescue operations
firefighting services
aerial survey companies
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:payload_capacity
|
400 kg
|
|
gptkbp:production_years
|
gptkb:1962
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:related_aircraft
|
gptkb:PZL-104_Wilga_35
PZL-104 Wilga 80 A
PZL-104 Wilga 80 B
PZL-104 Wilga 80 C
PZL-104 Wilga 80 D
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:stall_speed
|
65 km/h
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
general aviation
|
|
gptkbp:used_for
|
aerial work
|
|
gptkbp:variant
|
gptkb:PZL-104_Wilga_35
PZL-104 Wilga 80 A
PZL-104 Wilga 80 B
PZL-104 Wilga 80 C
PZL-104 Wilga 80 D
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.50 m
|
|
gptkbp:bfsParent
|
gptkb:PZL-104_Wilga
|
|
gptkbp:bfsLayer
|
7
|