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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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light aircraft
cantilever wing
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gptkbp:airlines
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FAA_certified
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gptkbp:avionics
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modern avionics systems available
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gptkbp:climbRate
|
1,200 ft/min
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gptkbp:cockpit
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glass cockpit option available
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gptkbp:controls
|
elevator, ailerons, rudder
yoke control
|
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gptkbp:countryOfOrigin
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gptkb:United_States
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|
gptkbp:covers
|
split flaps
|
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gptkbp:design
|
multi-engine training
low-wing design
Piper_Aircraft_design_team
|
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gptkbp:engine
|
2
Lycoming IO-360
|
|
gptkbp:engineType
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horizontally opposed
|
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gptkbp:firstFlight
|
1978
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gptkbp:fuelCapacity
|
110 gallons
|
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gptkbp:fuelType
|
avgas 100LL
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gptkbp:golfingEvents
|
10,000 ft
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gptkbp:height
|
8 ft 6 in
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-44 Seminole
|
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gptkbp:introduced
|
1978
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gptkbp:landingGear
|
tricycle gear
|
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gptkbp:length
|
28 ft 9 in
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gptkbp:maintenance
|
relatively low maintenance costs
|
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gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
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gptkbp:marketedAs
|
gptkb:Piper_Seminole
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gptkbp:marketSegment
|
general aviation
|
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gptkbp:maxSpeed
|
200 knots
|
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gptkbp:maxTakeoffWeight
|
3,800 lbs
|
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gptkbp:notableFeature
|
twin-engine configuration
|
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gptkbp:numberBuilt
|
over 1,000
|
|
gptkbp:operationalHistory
|
used by flight schools
|
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gptkbp:passengerCapacity
|
4
|
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gptkbp:performance
|
good performance in training scenarios
|
|
gptkbp:primaryMission
|
flight training
|
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gptkbp:propulsion
|
2
constant speed propellers
|
|
gptkbp:range
|
1,000 nautical miles
|
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gptkbp:rateOfFire
|
1,200 ft/min
|
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gptkbp:relatedAircraft
|
gptkb:Piper_PA-28R
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
15,000 ft
|
|
gptkbp:speed
|
170 knots
|
|
gptkbp:status
|
in production
|
|
gptkbp:takeoffDistance
|
1,500 ft
65 knots
|
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gptkbp:training
|
multi-engine training
|
|
gptkbp:type
|
twin-engine aircraft
|
|
gptkbp:weight
|
2,200 lbs
|
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gptkbp:wingArea
|
200 sq ft
|
|
gptkbp:wingspan
|
38 ft 4 in
|