|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-34_Seneca_XV
|
|
gptkbp:crew
|
1-2 pilots
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:fuel_capacity
|
100 gallons
|
|
gptkbp:height
|
9 ft 4 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-34 Seneca 200
|
|
gptkbp:introduced
|
gptkb:1971
|
|
gptkbp:is_popular_in
|
gptkb:Europe
gptkb:Australia
gptkb:North_America
|
|
gptkbp:is_used_by
|
charter services
flying schools
private owners
air taxi services
aircraft rental companies
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
28 ft 10 in
|
|
gptkbp:maintenance
|
requires regular inspections
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:marketed_as
|
gptkb:Seneca_II
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
4,300 lbs
|
|
gptkbp:notable_features
|
twin-engine configuration
|
|
gptkbp:performance
|
good climb rate
good fuel efficiency
stable flight characteristics
|
|
gptkbp:produced_by
|
over 3,000 units
|
|
gptkbp:production_years
|
1986-2004
1971-1983
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:role
|
personal and business travel
|
|
gptkbp:safety_record
|
generally good
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
18,000 ft
|
|
gptkbp:speed
|
170 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-34_Seneca_V
|
|
gptkbp:type
|
light twin aircraft
|
|
gptkbp:variant
|
gptkb:Piper_PA-34_Seneca_III
gptkb:Piper_PA-34_Seneca_IV
gptkb:Piper_PA-34_Seneca_V
Piper PA-34 Seneca I
|
|
gptkbp:weight
|
3,200 lbs
|
|
gptkbp:wingspan
|
38 ft 4 in
|