gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
3 hours
single-engine aircraft
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gptkbp:climb_rate
|
1,000 ft/min
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
gptkbp:cruise_speed
|
120 knots
|
gptkbp:design
|
Piper Aircraft design team
|
gptkbp:design_purpose
|
personal and business travel
|
gptkbp:engine_power
|
250 hp
|
gptkbp:engine_type
|
gptkb:turbofan_engine
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gptkbp:first_flight
|
1950
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gptkbp:flaps
|
manual flaps
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gptkbp:fuel_capacity
|
50 US gallons
|
gptkbp:fuel_type
|
aviation gasoline
|
gptkbp:fuselage_material
|
gptkb:metal
|
gptkbp:height
|
7 ft 0 in
|
gptkbp:historical_significance
|
part of Piper's post-war expansion.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-20 T
|
gptkbp:is_often_used_in
|
flight training, personal travel
|
gptkbp:landing_distance
|
1,000 ft
65 knots
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
24 ft 0 in
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
gptkbp:market_position
|
used aircraft market
|
gptkbp:market_segment
|
general aviation
|
gptkbp:max_speed
|
150 knots
|
gptkbp:max_takeoff_weight
|
2,400 lb
|
gptkbp:notable_features
|
gptkb:turbofan_engine
|
gptkbp:notable_pilots
|
private pilot license
|
gptkbp:number_built
|
approximately 1,000
|
gptkbp:offers_certificate
|
TC 3 A7
|
gptkbp:operational_history
|
used in private and commercial aviation
|
gptkbp:operational_range
|
600 nautical miles
|
gptkbp:passenger_capacity
|
gptkb:4
|
gptkbp:production_years
|
1950-1955
|
gptkbp:propeller
|
constant speed propeller
|
gptkbp:range
|
600 nautical miles
|
gptkbp:role
|
utility aircraft
|
gptkbp:service_ceiling
|
15,000 ft
|
gptkbp:stall_speed
|
60 knots
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:takeoff_distance
|
1,200 ft
|
gptkbp:variant
|
gptkb:Piper_PA-20
|
gptkbp:weight
|
1,500 lb
|
gptkbp:wing_area
|
200 sq ft
|
gptkbp:wing_configuration
|
high wing
|
gptkbp:wingspan
|
36 ft 0 in
|
gptkbp:bfsParent
|
gptkb:Piper_PA-20_Pacer
|
gptkbp:bfsLayer
|
7
|