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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gptkb:aircraft
single-engine aircraft
low-wing
private pilot license
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gptkbp:avionics
|
modern avionics systems
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gptkbp:certification
|
A1 SO
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gptkbp:cockpit
|
two-seat cockpit
|
gptkbp:community
|
popular among flying clubs
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gptkbp:design
|
Piper Aircraft design team
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gptkbp:engine
|
180 hp
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gptkbp:engine_type
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gptkb:Lycoming_IO-360
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gptkbp:first_flight
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gptkb:1967
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gptkbp:fuel_capacity
|
50 US gallons
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gptkbp:fuel_type
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gptkb:Avgas
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gptkbp:height
|
8 ft 6 in
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gptkbp:historical_significance
|
part of Piper's successful PA-28 series.
|
https://www.w3.org/2000/01/rdf-schema#label
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Piper PA-28 R Arrow 350
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gptkbp:introduced
|
gptkb:1970
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
24 ft 8 in
|
gptkbp:maintenance
|
relatively low maintenance costs
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gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
gptkbp:market_segment
|
private pilot training
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gptkbp:marketed_as
|
gptkb:Piper_Arrow
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gptkbp:material
|
metal and composite
|
gptkbp:max_speed
|
140 knots
|
gptkbp:max_takeoff_weight
|
2,550 lbs
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gptkbp:notable_features
|
retractable landing gear
|
gptkbp:number_built
|
over 2,000
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gptkbp:operational_history
|
used in flight schools
|
gptkbp:performance
|
good climb rate
|
gptkbp:primary_source
|
training and personal use
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gptkbp:production_location
|
gptkb:United_States
|
gptkbp:production_years
|
1967-1979
|
gptkbp:propulsion
|
variable-pitch propeller
|
gptkbp:range
|
700 nautical miles
|
gptkbp:role
|
general aviation
|
gptkbp:safety_record
|
generally good safety record
|
gptkbp:seating_capacity
|
gptkb:4
|
gptkbp:service_ceiling
|
15,000 ft
|
gptkbp:speed
|
120 knots
60 knots
|
gptkbp:successor
|
gptkb:Piper_PA-28_R_Arrow_IV
|
gptkbp:surface
|
elevator, ailerons, rudder
|
gptkbp:variant
|
gptkb:Piper_PA-28_Cherokee
|
gptkbp:weight
|
1,600 lbs
|
gptkbp:wing_area
|
174 sq ft
|
gptkbp:wingspan
|
36 ft 0 in
|