|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:climb_rate
|
700 ft/min
|
|
gptkbp:cockpit
|
side-by-side seating
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
120 knots
|
|
gptkbp:design
|
Piper Aircraft design team
|
|
gptkbp:engine_type
|
reciprocating engine
|
|
gptkbp:first_flight
|
gptkb:1949
|
|
gptkbp:flaps
|
manual 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 Super Cruiser
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
private flying
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
2,400 lb
|
|
gptkbp:notable_features
|
easy handling
low operating costs
good visibility
stable flight characteristics
|
|
gptkbp:offers_certificate
|
A-757
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:primary_use
|
general aviation
|
|
gptkbp:production_years
|
1949-1951
|
|
gptkbp:propeller
|
fixed-pitch propeller
|
|
gptkbp:range
|
600 miles
|
|
gptkbp:related_aircraft
|
gptkb:Piper_PA-22_Tri-Pacer
gptkb:Piper_PA-30_Twin_Comanche
gptkb:Piper_PA-28_Cherokee
gptkb:Piper_PA-24_Comanche
gptkb:Piper_PA-18_Super_Cub
|
|
gptkbp:role
|
gptkb:light_aircraft
|
|
gptkbp:stall_speed
|
50 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-22_Tri-Pacer
|
|
gptkbp:variant
|
Piper PA-20 B Super Cruiser
Piper PA-20 S Super Cruiser
|
|
gptkbp:weight
|
1,400 lb
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-20_H
gptkb:Piper_PA-20_K
gptkb:Piper_PA-20_Y
|
|
gptkbp:bfsLayer
|
8
|