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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_PA-28_R_Arrow
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gptkbp:aircraft_operated
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single-engine
low wing
10 feet 0 inches
4 feet 0 inches
15.5 lbs/sq ft
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gptkbp:avionics
|
varies by model
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|
gptkbp:category
|
general aviation
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|
gptkbp:certification
|
A1 SO
|
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gptkbp:cockpit
|
tandem seating
|
|
gptkbp:engine
|
gptkb:Lycoming
300 hp
horizontally opposed
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-540
IO-540-U4 A5
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
50 gallons
|
|
gptkbp:fuel_type
|
avgas
12-15 gallons/hour
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gptkbp:height
|
8 feet 6 inches
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28 R Arrow 300
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 feet 8 inches
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
private aviation
|
|
gptkbp:material
|
gptkb:NACA_2412
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 feet
1,500 feet
2,550 lbs
|
|
gptkbp:notable_features
|
retractable landing gear
|
|
gptkbp:number_built
|
over 3,000
|
|
gptkbp:power_consumption
|
8.5 lbs/hp
|
|
gptkbp:production_years
|
1967-1979
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
700 nautical miles
|
|
gptkbp:retired
|
gptkb:1979
|
|
gptkbp:seating_capacity
|
gptkb:4
1,000 lbs
|
|
gptkbp:service_ceiling
|
15,000 feet
|
|
gptkbp:speed
|
120 knots
60 knots
700 nautical miles
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
Piper PA-28
|
|
gptkbp:wing_area
|
174 square feet
|
|
gptkbp:wingspan
|
36 feet 0 inches
|
|
gptkbp:year_created
|
gptkb:1967
|