|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_support
|
certified
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:aircraft_type
|
fixed-wing
|
|
gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:cockpit
|
two seats in tandem
|
|
gptkbp:controls
|
yoke
|
|
gptkbp:cruise_speed
|
600 nautical miles
|
|
gptkbp:design
|
low-wing
Piper Aircraft engineers
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-540
|
|
gptkbp:first_flight
|
gptkb:1968
|
|
gptkbp:flight_deck
|
single pilot operation
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuel_type
|
avgas
|
|
gptkbp:height
|
8 ft 10 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-236 Dakota
|
|
gptkbp:introduced
|
gptkb:1968
|
|
gptkbp:is_popular_for
|
flight training
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 9 in
|
|
gptkbp:maintenance
|
relatively low cost
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
private and business aviation
|
|
gptkbp:marketed_as
|
gptkb:Dakota
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
2,800 lbs
|
|
gptkbp:notable_features
|
increased power and payload
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:passenger_capacity
|
gptkb:4
|
|
gptkbp:performance
|
good climb rate
|
|
gptkbp:production_years
|
1968-1982
|
|
gptkbp:propeller
|
variable-pitch
|
|
gptkbp:role
|
general aviation
|
|
gptkbp:service_ceiling
|
14,000 ft
|
|
gptkbp:stall_speed
|
60 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28-201_T
|
|
gptkbp:tail_type
|
N-number
|
|
gptkbp:training
|
used for private pilot training
|
|
gptkbp:type
|
single-engine
|
|
gptkbp:variant
|
gptkb:Piper_PA-28_series
|
|
gptkbp:weight
|
1,600 lbs
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Piper_28_R
|
|
gptkbp:bfsLayer
|
6
|