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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:aircraft
gptkb:Piper_Seneca
low-wing monoplane
twin-engine aircraft
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gptkbp:certification
|
A1 CE
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gptkbp:climb_rate
|
1,200 ft/min
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gptkbp:cockpit
|
tandem seating
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gptkbp:design
|
multi-purpose aircraft
Piper Aircraft design team
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gptkbp:discontinued
|
gptkb:1983
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gptkbp:elevation
|
10,000 ft
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gptkbp:engine
|
2
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gptkbp:engine_type
|
gptkb:Lycoming_IO-360
piston engine
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gptkbp:first_flight
|
gptkb:1971
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gptkbp:fuel_capacity
|
100 gallons
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gptkbp:fuel_type
|
avgas
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gptkbp:height
|
9 ft 4 in
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https://www.w3.org/2000/01/rdf-schema#label
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Piper PA-34-200 T Seneca II
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gptkbp:is_designed_to
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general aviation
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gptkbp:is_often_used_in
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flight training
personal transport
air taxi
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
28 ft 10 in
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gptkbp:manufacturer
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gptkb:Piper_Aircraft
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gptkbp:market_segment
|
light twin aircraft
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gptkbp:max_speed
|
200 knots
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gptkbp:max_takeoff_weight
|
4,000 lbs
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gptkbp:notable_features
|
twin-engine design
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gptkbp:notable_users
|
flying schools
charter companies
private owners
aircraft rental companies
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gptkbp:produced_by
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1,000 units
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gptkbp:production_years
|
1971-1983
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gptkbp:propulsion
|
constant speed propeller
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gptkbp:range
|
1,200 nautical miles
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gptkbp:related_model
|
gptkb:Seneca_II
|
|
gptkbp:seating_capacity
|
gptkb:6
1,200 lbs
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|
gptkbp:service_ceiling
|
18,000 ft
|
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gptkbp:speed
|
170 knots
60 knots
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gptkbp:successor
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gptkb:Piper_PA-34-220_T_Seneca_III
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gptkbp:weight
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2,800 lbs
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gptkbp:wing_area
|
200 sq ft
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gptkbp:wingspan
|
38 ft 4 in
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gptkbp:year_created
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gptkb:1971
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gptkbp:bfsParent
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gptkb:No._3_Group_RAF
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gptkbp:bfsLayer
|
4
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