|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-28_R_Arrow
|
|
gptkbp:aircraft_operated
|
gptkb:Piper_PA-28_R_Arrow_II
gptkb:Piper_PA-28_R_Arrow_IV
gptkb:aircraft
gptkb:Piper_PA-28_Cherokee
low-wing
N-number
|
|
gptkbp:avionics
|
modern avionics systems
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:controls
|
yoke control
|
|
gptkbp:design
|
low-wing monoplane
Piper Aircraft design team
|
|
gptkbp:engine
|
Lycoming IO-360-B1 G6
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-360
|
|
gptkbp:first_flight
|
gptkb:1967
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuel_type
|
avgas
|
|
gptkbp:height
|
8 ft 6 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28 R Arrow 450
|
|
gptkbp:introduced
|
gptkb:1967
|
|
gptkbp:is_popular_in
|
gptkb:North_America
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 8 in
|
|
gptkbp:maintenance
|
requires regular maintenance checks
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
private pilots
|
|
gptkbp:marketed_as
|
gptkb:Piper_Arrow
|
|
gptkbp:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
2,550 lb
|
|
gptkbp:notable_features
|
retractable landing gear
|
|
gptkbp:number_built
|
over 5,000
|
|
gptkbp:operational_history
|
used in flight training
|
|
gptkbp:performance
|
good performance for cross-country flying
|
|
gptkbp:predecessor
|
gptkb:Piper_PA-28_R_Arrow_II
|
|
gptkbp:production_years
|
1967-1977
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:role
|
general aviation
|
|
gptkbp:safety_record
|
generally good safety record
|
|
gptkbp:seating_capacity
|
gptkb:4
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:speed
|
600 nautical miles
60 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28_R_Arrow_IV
|
|
gptkbp:type
|
single-engine
|
|
gptkbp:variant
|
Piper PA-28
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|