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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
low wing
|
|
gptkbp:avionics
|
varies by installation
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:design
|
low-wing monoplane
Piper_Aircraft_design_team
|
|
gptkbp:engine
|
1
|
|
gptkbp:enginePower
|
235 hp
|
|
gptkbp:engineType
|
Lycoming IO-540
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuelCapacity
|
50 US gallons
|
|
gptkbp:golfingEvents
|
600 nautical miles
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8 ft 6 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-236 Dakota
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:marketedAs
|
Dakota
|
|
gptkbp:marketSegment
|
private and business aviation
|
|
gptkbp:maximum_speed
|
140 knots
|
|
gptkbp:maxTakeoffWeight
|
2,800 lbs
|
|
gptkbp:notableFeature
|
retractable landing gear
|
|
gptkbp:numberBuilt
|
over 32,000
|
|
gptkbp:passengerCapacity
|
4
|
|
gptkbp:productionYears
|
1970-1982
|
|
gptkbp:products
|
A1SO
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:relatedModel
|
gptkb:Piper_PA-28_series
|
|
gptkbp:role
|
general aviation
|
|
gptkbp:services
|
14,000 ft
|
|
gptkbp:speed
|
120 knots
60 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28-201T_Turbo_Dakota
|
|
gptkbp:takeoffDistance
|
1,200 ft
1,500 ft
|
|
gptkbp:weight
|
1,600 lbs
|
|
gptkbp:wingArea
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:yearEstablished
|
1970
|