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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Piper_PA-28_R_Arrow
|
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gptkbp:aircraft_operated
|
gptkb:aircraft
single-engine aircraft
low wing
|
|
gptkbp:avionics
|
basic VFR instruments
|
|
gptkbp:certification
|
A1 SO
|
|
gptkbp:climb_rate
|
700 feet per minute
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
general aviation
|
|
gptkbp:elevation
|
14,000 feet
|
|
gptkbp:engine
|
gptkb:musical
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-360
Lycoming IO-360-B1 G6
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
50 gallons
|
|
gptkbp:fuel_type
|
Avgas 100 LL
|
|
gptkbp:height
|
8 feet 6 inches
|
|
gptkbp:historical_significance
|
popular trainer aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28 R Arrow 235
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 feet 8 inches
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
private and training use
|
|
gptkbp:max_speed
|
135 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 feet
1,500 feet
2,550 lbs
|
|
gptkbp:notable_features
|
retractable landing gear
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:produced_by
|
over 2,000 units
|
|
gptkbp:production_years
|
1967-1979
|
|
gptkbp:propulsion
|
gptkb:musical
constant speed propeller
|
|
gptkbp:range
|
700 nautical miles
|
|
gptkbp:rate_of_fire
|
10 gallons per hour
|
|
gptkbp:seating_capacity
|
gptkb:4
1,000 lbs
|
|
gptkbp:service_ceiling
|
14,000 feet
|
|
gptkbp:speed
|
120 knots
60 knots
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:variant
|
gptkb:Piper_PA-28_Cherokee
|
|
gptkbp:wing_area
|
174 square feet
|
|
gptkbp:wingspan
|
36 feet 0 inches
|
|
gptkbp:year_created
|
gptkb:1967
|