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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Piper_Cherokee
gptkb:Piper_PA-28-161
|
|
gptkbp:aircraft_operated
|
gptkb:Piper_PA-28-181
gptkb:Piper_PA-28-200
gptkb:aircraft
gptkb:Piper_PA-28-235
gptkb:Piper_PA-28-140
gptkb:Piper_PA-28-161
civil aircraft
|
|
gptkbp:category
|
general aviation
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
Piper Aircraft design team
|
|
gptkbp:engine
|
gptkb:Lycoming_IO-360
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1968
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuel_type
|
avgas
|
|
gptkbp:height
|
8 ft 6 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-201
|
|
gptkbp:introduced
|
gptkb:1977
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:marketed_as
|
gptkb:Cherokee_201
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
2,550 lb
|
|
gptkbp:notable_features
|
low-wing design
|
|
gptkbp:operational_history
|
used for training and personal flying.
|
|
gptkbp:produced_by
|
1,000 units
|
|
gptkbp:production_years
|
1977-2000
|
|
gptkbp:propulsion
|
constant-speed propeller
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:retired
|
gptkb:2000
|
|
gptkbp:seating_capacity
|
gptkb:3
1,000 lb
|
|
gptkbp:service_ceiling
|
14,000 ft
|
|
gptkbp:speed
|
55 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28-236
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:trademark
|
gptkb:Piper_Cherokee
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:variant
|
Piper PA-28
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|