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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:light_aircraft
N-number
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gptkbp:climb_rate
|
700 ft/min
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|
gptkbp:cockpit
|
two-seat configuration
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gptkbp:crew
|
gptkb:1
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gptkbp:cruise_speed
|
120 knots
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gptkbp:design
|
low-wing monoplane
Piper Aircraft design team
|
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gptkbp:engine_type
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gptkb:Lycoming_O-320
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gptkbp:first_flight
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gptkb:1966
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|
gptkbp:flaps
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gptkb:manual
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|
gptkbp:fuel_capacity
|
50 US gallons
|
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gptkbp:fuel_type
|
avgas
|
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gptkbp:fuselage_material
|
gptkb:NACA_2412
|
|
gptkbp:height
|
8 ft 6 in
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gptkbp:historical_significance
|
popular trainer aircraft
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|
https://www.w3.org/2000/01/rdf-schema#label
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Piper PA-28-151 Warrior
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gptkbp:introduced
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gptkb:1970
|
|
gptkbp:is_often_used_in
|
private flying
|
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gptkbp:landing_distance
|
1,200 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
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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:max_speed
|
140 knots
|
|
gptkbp:max_takeoff_weight
|
2,550 lbs
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|
gptkbp:notable_users
|
flying schools
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|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:offers_certificate
|
A1 SO
|
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gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:payload_capacity
|
950 lbs
|
|
gptkbp:power_output
|
150 hp
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:production_years
|
1970-1982
|
|
gptkbp:propeller
|
fixed-pitch
|
|
gptkbp:range
|
600 nautical miles
|
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gptkbp:related_model
|
gptkb:Piper_PA-28-180
gptkb:Piper_PA-28-140
gptkb:Piper_PA-28-161
|
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gptkbp:service_ceiling
|
12,000 ft
|
|
gptkbp:stall_speed
|
50 knots
|
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gptkbp:successor
|
gptkb:Piper_PA-28-161_Warrior_II
|
|
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
|
1,600 lbs
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wing_configuration
|
straight wing
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gptkbp:wingspan
|
36 ft 0 in
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gptkbp:bfsParent
|
gptkb:Piper_Warrior
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gptkbp:bfsLayer
|
7
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