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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
1,200 miles
low-wing
multi-engine land
|
|
gptkbp:airlines
|
1-2 pilots
|
|
gptkbp:avionics
|
modern avionics systems
|
|
gptkbp:category
|
light aircraft
|
|
gptkbp:climbRate
|
1,200 ft/min
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:commonName
|
flight training, personal use
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
1-2 pilots
|
|
gptkbp:design
|
Piper_Aircraft_design_team
|
|
gptkbp:engine
|
2
|
|
gptkbp:engineConfiguration
|
horizontally opposed
|
|
gptkbp:engineType
|
Lycoming IO-360
|
|
gptkbp:firstFlight
|
1971
|
|
gptkbp:fuelCapacity
|
100 gallons
|
|
gptkbp:fuelType
|
avgas
|
|
gptkbp:height
|
9 ft 4 in
|
|
gptkbp:historicalSignificance
|
part_of_Piper's_twin-engine_lineup.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-34-200T Seneca II
|
|
gptkbp:introduced
|
1971
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
28 ft 10 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market
|
popular among private pilots
|
|
gptkbp:marketSegment
|
light twin aircraft
|
|
gptkbp:maximumDepth
|
1,200 lbs
|
|
gptkbp:maxSpeed
|
200 knots
|
|
gptkbp:maxTakeoffWeight
|
3,800 lbs
|
|
gptkbp:notableFeature
|
twin-engine
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:passengerCapacity
|
6
|
|
gptkbp:performance
|
good climb performance
|
|
gptkbp:productionYears
|
1971-1983
|
|
gptkbp:products
|
A1EA
|
|
gptkbp:propulsion
|
constant speed
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:retired
|
1983
|
|
gptkbp:safetyFeatures
|
dual controls, emergency systems
|
|
gptkbp:services
|
18,000 ft
|
|
gptkbp:speed
|
170 knots
60 knots
|
|
gptkbp:takeoffDistance
|
1,600 ft
70 knots
1,800 ft
|
|
gptkbp:usedFor
|
general aviation
|
|
gptkbp:variant
|
gptkb:Piper_Seneca
|
|
gptkbp:wingArea
|
200 sq ft
|
|
gptkbp:wingspan
|
38 ft 4 in
|