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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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gptkb:Piper_PA-28_family
fixed-wing aircraft
light aircraft
utility aircraft
single-engine
70 kg/m²
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gptkbp:avionics
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basic_VFR_instruments
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gptkbp:climbRate
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1,000 ft/min
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gptkbp:cockpit
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tandem_seating
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gptkbp:commonName
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flight training, personal use
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gptkbp:constructionMaterial
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NACA 2412
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gptkbp:controls
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elevator, ailerons, rudder
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gptkbp:covers
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split flaps
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gptkbp:crew
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1
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gptkbp:design
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trainer aircraft
Piper_Aircraft_design_team
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gptkbp:engine
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IO-360
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gptkbp:engineConfiguration
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Lycoming
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gptkbp:engineType
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piston engine
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gptkbp:firstFlight
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1961
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gptkbp:fuelCapacity
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50 US gallons
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gptkbp:fuelType
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Avgas
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gptkbp:height
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2.54 m
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gptkbp:historicalSignificance
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popular trainer in the 1960s and 1970s
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|
https://www.w3.org/2000/01/rdf-schema#label
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PA-28-200
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gptkbp:landingGear
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tricycle 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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1961
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gptkbp:marketSegment
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general aviation
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gptkbp:maxSpeed
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140 knots
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gptkbp:maxTakeoffWeight
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1,134 kg
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gptkbp:notableFeature
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low-wing design
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gptkbp:numberBuilt
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over 1,000
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gptkbp:passengerCapacity
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3
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gptkbp:powerOutput
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200 hp
5.7 kg/hp
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gptkbp:productionYears
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1961-1977
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gptkbp:products
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A1EA
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gptkbp:propulsion
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fixed-pitch propeller
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gptkbp:range
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600 nautical miles
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gptkbp:relatedModel
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PA-28-161,_PA-28-181
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gptkbp:revenue
|
1977
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gptkbp:safetyFeatures
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dual controls
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gptkbp:services
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12,000 ft
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gptkbp:speed
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50 knots
120 knots
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gptkbp:takeoffDistance
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500 m
600 m
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gptkbp:variant
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gptkb:Piper_PA-28_Cherokee
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gptkbp:weight
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750 kg
384 kg
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gptkbp:wingArea
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16.2 m²
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gptkbp:wingspan
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8.23 m
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