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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
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1,200 km
light aircraft
trainer aircraft
straight wing
73.5 kg/m²
trainer and personal use
single-engine_piston_aircraft
|
|
gptkbp:avionics
|
basic navigation equipment
|
|
gptkbp:capacity
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4
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gptkbp:category
|
general aviation
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gptkbp:cockpit
|
two-seat cockpit
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gptkbp:constructionMaterial
|
all-metal construction
|
|
gptkbp:controls
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elevator, ailerons, rudder
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|
gptkbp:crew
|
1
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|
gptkbp:design
|
low-wing monoplane
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|
gptkbp:engine
|
gptkb:Lycoming_O-360-A4M
|
|
gptkbp:engineConfiguration
|
horizontally opposed
|
|
gptkbp:enginePower
|
180 hp
|
|
gptkbp:engineType
|
Lycoming O-360
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|
gptkbp:famousFor
|
flight training
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
50 US gallons
12 US gallons per hour
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.67 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-161 Warrior II
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
7.34 m
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market
|
civil aviation
|
|
gptkbp:maxSpeed
|
140 knots
|
|
gptkbp:maxTakeoffWeight
|
1,157 kg
|
|
gptkbp:notableFeature
|
stable flight characteristics
|
|
gptkbp:numberBuilt
|
over 2,000
|
|
gptkbp:powerOutput
|
6.4 kg/hp
|
|
gptkbp:productionYears
|
1974-1986
|
|
gptkbp:propulsion
|
fixed-pitch
two-blade propeller
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:services
|
14,000 ft
|
|
gptkbp:speed
|
54 knots
126 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-28-161_Warrior_III
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:variant
|
gptkb:Piper_PA-28-161_Warrior
|
|
gptkbp:weight
|
750 kg
407 kg
|
|
gptkbp:wingArea
|
16.2 m²
|
|
gptkbp:wingspan
|
11.95 m
|