PZL-101 Gawron

URI: https://gptkb.org/entity/PZL-101_Gawron
GPTKB entity
Statements (43)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aerobatic yes
gptkbp:aircraft_configuration low-wing monoplane
gptkbp:aircraft_operated general aviation
gptkbp:aircraft_type gptkb:training
gptkbp:climb_rate 5 m/s
gptkbp:cockpit tandem cockpit
gptkbp:country_of_origin gptkb:Poland
gptkbp:crew gptkb:1
gptkbp:design PZL designers
gptkbp:engine_type piston engine
gptkbp:first_flight gptkb:1984
gptkbp:floors conventional tail
gptkbp:fuel_capacity 120 L
https://www.w3.org/2000/01/rdf-schema#label PZL-101 Gawron
gptkbp:introduced gptkb:1984
gptkbp:landing_distance 400 m
gptkbp:landing_gear tricycle gear
gptkbp:length 8.2 m
gptkbp:manufacturer PZL
gptkbp:max_speed 250 km/h
gptkbp:max_takeoff_weight 1,200 kg
gptkbp:number_built 50
gptkbp:power_source gptkb:Lycoming_O-360
gptkbp:production_years gptkb:1984
gptkb:1990
gptkbp:propeller two-bladed propeller
gptkbp:range 1,000 km
gptkbp:role gptkb:trainer_aircraft
gptkb:light_aircraft
gptkbp:rollout_distance 200 m
gptkbp:service_ceiling 4,500 m
gptkbp:stall_speed 65 km/h
gptkbp:status retired
gptkbp:takeoff_distance 300 m
gptkbp:training pilot training
gptkbp:type civil aircraft
gptkbp:used_by gptkb:Polish_Air_Force
gptkbp:variant PZL-101 Gawron II
gptkbp:wing_area 12.5 m²
gptkbp:wingspan 10.5 m
gptkbp:bfsParent gptkb:PZL-104_Wilga
gptkbp:bfsLayer 7