|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:trainer_aircraft
gptkb:light_aircraft
fixed-wing aircraft
single-engine aircraft
utility aircraft
civil aircraft
business aircraft
touring aircraft
tailwheel aircraft
recreational aircraft
|
|
gptkbp:climb_rate
|
800 ft/min
|
|
gptkbp:cockpit
|
two seats side by side
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:cruise_speed
|
120 knots
|
|
gptkbp:design
|
gptkb:Piper_Aircraft_Company
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1950
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
36 US gallons
|
|
gptkbp:height
|
7 ft 0 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-20 J
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
150 knots
|
|
gptkbp:max_takeoff_weight
|
2,400 lb
|
|
gptkbp:notable_features
|
low stall speed
|
|
gptkbp:number_built
|
1,000+
|
|
gptkbp:operational_history
|
used in flight training
used for agricultural purposes
used for personal flying
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:production_years
|
1950-1954
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:service_ceiling
|
14,000 ft
|
|
gptkbp:successor
|
gptkb:Piper_PA-22
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:variant
|
gptkb:Piper_PA-20
|
|
gptkbp:weight
|
1,400 lb
|
|
gptkbp:wing_configuration
|
high wing
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-20_Pacer
|
|
gptkbp:bfsLayer
|
7
|