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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_operated
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gptkb:light_aircraft
multi-engine aircraft
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gptkbp:aircraft_role
|
utility aircraft
|
|
gptkbp:avionics
|
gptkb:GPS
gptkb:radio_station
gptkb:Racing
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
gptkb:elevator
rudder
aileron
|
|
gptkbp:control_system
|
yoke
|
|
gptkbp:cruise_speed
|
170 knots
|
|
gptkbp:design
|
Piper Aircraft design team
|
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gptkbp:engine_configuration
|
horizontally opposed
|
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gptkbp:engine_type
|
gptkb:Lycoming_IO-540
Lycoming IO-540-U2 A5
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:flaps
|
split flaps
|
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gptkbp:fuel_capacity
|
80 US gallons
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gptkbp:fuel_type
|
avgas
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gptkbp:fuselage_material
|
low-wing
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gptkbp:height
|
8 ft 6 in
|
|
gptkbp:historical_significance
|
popular in the 1960s and 1970s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper Aztec PA-23-250 C
|
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gptkbp:intended_use
|
general aviation
|
|
gptkbp:is_often_used_in
|
cargo transport
charter flights
flight training
personal travel
|
|
gptkbp:landing_gear
|
retractable
tricycle gear
|
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gptkbp:length
|
27 ft 0 in
|
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gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
5,000 lbs
|
|
gptkbp:notable_features
|
twin-engine design
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:offers_certificate
|
A2 PC
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:production_location
|
gptkb:Vero_Beach,_Florida
|
|
gptkbp:production_years
|
1960-1982
|
|
gptkbp:propeller
|
2
constant speed
|
|
gptkbp:range
|
1,200 nautical miles
|
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gptkbp:related_aircraft
|
gptkb:Piper_Seminole
gptkb:Piper_Navajo
gptkb:Piper_Aztec_PA-23-260
Piper Aztec family
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:variant
|
PA-23-250
|
|
gptkbp:weight
|
3,200 lbs
|
|
gptkbp:wingspan
|
38 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Piper_Aztec_PA-23-250
|
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gptkbp:bfsLayer
|
7
|