gptkbp:instance_of
|
gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:light_aircraft
N-number
good handling characteristics
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gptkbp:aircraft_type
|
gptkb:civil_aviation
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
gptkbp:country_of_origin
|
gptkb:United_States
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gptkbp:crew
|
1-2 pilots
|
gptkbp:cruise_speed
|
120 knots
600 nautical miles
|
gptkbp:design
|
gptkb:Piper_Aircraft_Company
|
gptkbp:engine_power
|
180 hp
|
gptkbp:engine_type
|
gptkb:Lycoming_O-360
|
gptkbp:first_flight
|
gptkb:1960
|
gptkbp:flaps
|
split flaps
|
gptkbp:fuel_capacity
|
50 US gallons
|
gptkbp:fuel_type
|
avgas
|
gptkbp:fuselage_material
|
gptkb:metal
|
gptkbp:height
|
8 ft 6 in
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gptkbp:historical_significance
|
popular trainer aircraft.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-180
|
gptkbp:introduced
|
gptkb:1961
|
gptkbp:is_often_used_in
|
flight training
|
gptkbp:landing_distance
|
1,200 ft
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
24 ft 0 in
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
gptkbp:market_segment
|
private flying
|
gptkbp:max_speed
|
138 knots
|
gptkbp:max_takeoff_weight
|
2,550 lb
|
gptkbp:military_lessons
|
yes
|
gptkbp:notable_features
|
low-wing design
|
gptkbp:notable_users
|
flying clubs
|
gptkbp:number_built
|
over 32,000
|
gptkbp:orbital_altitude
|
8,000 ft
|
gptkbp:passenger_capacity
|
gptkb:4
|
gptkbp:payload_capacity
|
1,000 lb
|
gptkbp:production_years
|
1961-1977
|
gptkbp:propeller
|
fixed-pitch propeller
|
gptkbp:range
|
700 miles
|
gptkbp:role
|
general aviation
|
gptkbp:service_ceiling
|
13,000 ft
|
gptkbp:stall_speed
|
54 knots
|
gptkbp:tail_type
|
conventional tail
|
gptkbp:takeoff_distance
|
1,500 ft
|
gptkbp:type
|
single-engine aircraft
|
gptkbp:variant
|
gptkb:Piper_PA-28_Cherokee
|
gptkbp:weight
|
1,500 lb
|
gptkbp:wing_area
|
174 sq ft
|
gptkbp:wing_configuration
|
low-wing
|
gptkbp:wingspan
|
36 ft 0 in
|
gptkbp:bfsParent
|
gptkb:Martinique_Air_Force
|
gptkbp:bfsLayer
|
5
|