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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
|
|
gptkbp:aircraft_operated
|
gptkb:Piper_PA-28_family
low-wing
low-wing monoplane
|
|
gptkbp:avionics
|
basic VFR avionics
|
|
gptkbp:category
|
general aviation
|
|
gptkbp:climb_rate
|
1,000 ft/min
|
|
gptkbp:cockpit
|
two-seat cockpit configuration
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
Piper Aircraft design team
|
|
gptkbp:engine
|
gptkb:musical
180 hp
horizontally opposed
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-360
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:flaps
|
manual flaps
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuel_type
|
avgas 100 LL
|
|
gptkbp:height
|
8 ft 6 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28 R Arrow 950
|
|
gptkbp:introduced
|
gptkb:1967
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 8 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
gptkb:aircraft
|
|
gptkbp:marketed_as
|
gptkb:Piper_Arrow
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 ft
1,500 ft
2,550 lbs
|
|
gptkbp:notable_features
|
retractable landing gear
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:primary_source
|
personal and business flying
|
|
gptkbp:produced_by
|
over 2,000 units
|
|
gptkbp:production_years
|
1967-1979
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
700 nautical miles
|
|
gptkbp:retired
|
gptkb:1979
|
|
gptkbp:seating_capacity
|
1,000 lbs
3 passengers
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:speed
|
120 knots
60 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28_R_Arrow_IV
|
|
gptkbp:supports
|
certified for VFR and IFR
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:weight
|
1,500 lbs
1,050 lbs
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|