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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Peruvian_Air_Force
|
|
gptkbp:aircraft_operated
|
general aviation
utility aircraft
low-wing
12 ft 0 in
twin-engine aircraft
4 ft 0 in
20 lb/sq ft
Piper Seneca family
|
|
gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:certification
|
A1 EA
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
Piper Aircraft design team
|
|
gptkbp:engine
|
2
200 hp
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-360
piston engine
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:fuel_capacity
|
100 US gallons
|
|
gptkbp:fuel_type
|
avgas
|
|
gptkbp:height
|
9 ft 4 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-34 Seneca XV
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
28 ft 10 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
light aircraft market
|
|
gptkbp:marketed_as
|
gptkb:Seneca_XV
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 ft
1,500 ft
4,200 lb
|
|
gptkbp:notable_users
|
private pilots
|
|
gptkbp:operational_history
|
used for training and personal transport.
|
|
gptkbp:power_consumption
|
21 lb/hp
|
|
gptkbp:produced_by
|
200 units
|
|
gptkbp:production_years
|
1980-1983
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:role
|
light twin aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
1,200 lb
|
|
gptkbp:service_ceiling
|
18,000 ft
|
|
gptkbp:speed
|
180 knots
60 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-34_Seneca_200
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:variant
|
gptkb:Piper_PA-34_Seneca
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wingspan
|
38 ft 0 in
|