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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
|
gptkb:Lycoming_O-360
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gptkbp:aircraft_operated
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gptkb:aircraft
single-engine
low-wing monoplane
10 ft 0 in
4 ft 0 in
15 lbs/sq ft
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gptkbp:certification
|
A1 SO
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gptkbp:climb_rate
|
700 ft/min
|
|
gptkbp:cockpit
|
side-by-side seating
|
|
gptkbp:controls
|
yoke
|
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gptkbp:design
|
gptkb:Piper_Aircraft_Company
|
|
gptkbp:elevation
|
8,000 ft
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gptkbp:engine
|
140 hp
front-mounted
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gptkbp:engine_type
|
gptkb:Lycoming_O-320
|
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gptkbp:first_flight
|
gptkb:1961
|
|
gptkbp:flaps
|
single-slot flaps
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gptkbp:fuel_capacity
|
50 gallons
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gptkbp:fuel_type
|
avgas
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gptkbp:height
|
8 ft 6 in
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper 28-140
|
|
gptkbp:is_often_used_in
|
training and personal flying
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
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|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
general aviation
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gptkbp:marketed_as
|
Cherokee 140
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gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
120 knots
|
|
gptkbp:max_takeoff_weight
|
1,500 ft
60 knots
2,550 lbs
|
|
gptkbp:notable_features
|
low-wing design
|
|
gptkbp:number_built
|
over 5,000
|
|
gptkbp:power_consumption
|
10 lbs/hp
|
|
gptkbp:production_years
|
1961-1977
|
|
gptkbp:propulsion
|
fixed-pitch
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:seating_capacity
|
gptkb:4
200 lbs
1,000 lbs
|
|
gptkbp:service_ceiling
|
12,000 ft
|
|
gptkbp:service_history
|
used for flight training and personal use.
|
|
gptkbp:speed
|
docile
50 knots
500 nautical miles
100 knots
75% power
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
gptkb:Piper_PA-28_Cherokee
|
|
gptkbp:weight
|
1,500 lbs
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|