|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
low-wing
|
|
gptkbp:aircraft_operated
|
4 hours
modern navigation systems
reliable and efficient
multi-engine land
|
|
gptkbp:aircraft_role
|
personal transport
|
|
gptkbp:aircraft_type
|
gptkb:civil_aviation
|
|
gptkbp:climb_rate
|
1,200 ft/min
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cruise_speed
|
160 knots
170 knots
|
|
gptkbp:design
|
light twin aircraft
Piper Aircraft design team
|
|
gptkbp:elevation
|
25,000 ft
|
|
gptkbp:engine_configuration
|
horizontally opposed
|
|
gptkbp:engine_power
|
180 hp
|
|
gptkbp:engine_type
|
gptkb:Lycoming_IO-360
piston engine
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:flaps
|
single slotted flap
|
|
gptkbp:fuel_capacity
|
100 gallons
|
|
gptkbp:fuel_type
|
avgas
|
|
gptkbp:height
|
9 ft 4 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-34 Seneca V
|
|
gptkbp:interior_features
|
configurable seating
|
|
gptkbp:introduced
|
gptkb:1971
|
|
gptkbp:is_often_used_in
|
general aviation
|
|
gptkbp:landing_distance
|
1,500 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
28 ft 9 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
gptkb:light_aircraft
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
4,200 lb
|
|
gptkbp:notable_features
|
twin-engine configuration
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:offers_certificate
|
A1 CE
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:payload_capacity
|
1,200 lb
|
|
gptkbp:production_location
|
gptkb:United_States
|
|
gptkbp:production_years
|
1971-2009
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:range
|
1,200 miles
1,200 nautical miles
|
|
gptkbp:related_aircraft
|
gptkb:Piper_Seneca
|
|
gptkbp:service_ceiling
|
18,000 ft
|
|
gptkbp:squadrons
|
various
|
|
gptkbp:stall_speed
|
65 knots
|
|
gptkbp:successor
|
gptkb:Piper_PA-34_Seneca_VI
|
|
gptkbp:takeoff_distance
|
2,000 ft
|
|
gptkbp:typical_load_factor
|
+3.8g to -1.5g
|
|
gptkbp:variant
|
Seneca I, II, III, IV, V
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:weight_max_landing
|
3,800 lb
|
|
gptkbp:weight_max_ramp
|
4,200 lb
|
|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wingspan
|
38 ft 4 in
|
|
gptkbp:bfsParent
|
gptkb:Peruvian_Air_Force
gptkb:Brazilian_Air_Force
gptkb:No._10_Group_RAF
gptkb:South_Vietnam_Air_Force
|
|
gptkbp:bfsLayer
|
5
|