gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
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gptkb:Piper_Cherokee
gptkb:Piper_PA-28-161
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gptkbp:aircraft_operated
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gptkb:Piper_PA-28_family
1,500 lbs
single-engine aircraft
8 ft 4 in
low-wing monoplane
two-blade propeller
24 ft 1 in
cantilever wing
138 mph
training and personal use
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gptkbp:avionics
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varies by model
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gptkbp:category
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gptkb:aircraft
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gptkbp:controls
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mechanical control system
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gptkbp:crew
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gptkb:musical
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gptkbp:design
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low-wing design
Piper Aircraft design team
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gptkbp:engine
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gptkb:musical
gptkb:Lycoming_IO-540
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gptkbp:engine_type
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piston engine
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gptkbp:first_flight
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gptkb:1961
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gptkbp:fuel_capacity
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50 US gallons
50 gallons
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gptkbp:fuel_type
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avgas
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gptkbp:height
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2.54 m
|
https://www.w3.org/2000/01/rdf-schema#label
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Piper PA-28-235
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gptkbp:landing_gear
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tricycle gear
tricycle landing gear
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gptkbp:length
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7.34 m
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gptkbp:manufacturer
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gptkb:Piper_Aircraft
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gptkbp:market
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private and flight training
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gptkbp:marketed_as
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gptkb:Piper_Cherokee_235
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gptkbp:material
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monocoque construction
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gptkbp:max_speed
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140 knots
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gptkbp:max_takeoff_weight
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1,157 kg
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gptkbp:nickname
|
gptkb:Cherokee_235
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gptkbp:notable_features
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four-seat capacity
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gptkbp:power_output
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235 hp
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gptkbp:produced_by
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over 1,000 units
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gptkbp:production_years
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1961-1977
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gptkbp:propulsion
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fixed-pitch propeller
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gptkbp:range
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700 miles
600 nautical miles
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gptkbp:seating_capacity
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gptkb:3
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gptkbp:service_ceiling
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14,000 ft
14,000 feet
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gptkbp:setting
|
low-wing monoplane
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gptkbp:speed
|
120 knots
55 knots
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gptkbp:successor
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gptkb:Piper_PA-28-236
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gptkbp:surface
|
elevator, ailerons, rudder
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gptkbp:tail_type
|
conventional tail
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gptkbp:type
|
general aviation aircraft
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gptkbp:variant
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gptkb:Piper_PA-28-200
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gptkbp:weight
|
680 kg
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gptkbp:wing_area
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16.2 m²
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gptkbp:wingspan
|
10.67 m
34 ft 11 in
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