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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
|
twin-seat configuration
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gptkbp:aircraft_operated
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gptkb:light_aircraft
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gptkbp:aircraft_role
|
training and light utility
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gptkbp:aircraft_type
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gptkb:training
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gptkbp:armament
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gptkb:none
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gptkbp:availability
|
used by various flight schools
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gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
tandem seating
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gptkbp:cockpit_instruments
|
modern avionics
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gptkbp:crew
|
2
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gptkbp:design
|
low-wing monoplane
PZL Mielec design team
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gptkbp:design_features
|
high visibility cockpit
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gptkbp:engine
|
PZL-120
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gptkbp:engine_type
|
piston engine
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gptkbp:first_delivery
|
gptkb:1994
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gptkbp:first_flight
|
gptkb:1993
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gptkbp:fuel_capacity
|
200 L
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|
https://www.w3.org/2000/01/rdf-schema#label
|
PZL-120 Sokol
|
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gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:PZL_Mielec
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|
gptkbp:market
|
primarily in Europe
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|
gptkbp:max_speed
|
250 km/h
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|
gptkbp:max_takeoff_weight
|
1,200 kg
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gptkbp:number_built
|
50
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gptkbp:operational_history
|
used in various air forces
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gptkbp:payload_capacity
|
400 kg
|
|
gptkbp:performance
|
good maneuverability
|
|
gptkbp:primary_user
|
gptkb:Polish_Air_Force
|
|
gptkbp:production_years
|
1993-2000
|
|
gptkbp:propeller
|
variable pitch propeller
|
|
gptkbp:provides_training_for
|
aerobatics training
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:related_aircraft
|
gptkb:PZL-130_Orlik
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:training_programs
|
initial pilot training
|
|
gptkbp:type
|
civil and military training aircraft
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingspan
|
9.5 m
|
|
gptkbp:bfsParent
|
gptkb:PZL-104_Wilga
|
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gptkbp:bfsLayer
|
7
|