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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:climb_rate
|
1,200 ft/min
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
170 knots
|
|
gptkbp:design
|
Piper Aircraft design team
|
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gptkbp:engine_type
|
gptkb:Lycoming_IO-540
piston engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
80 US gallons
|
|
gptkbp:height
|
8 ft 6 in
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper Aztec PA-23-260 C
|
|
gptkbp:introduced
|
gptkb:1960
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
27 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
gptkb:light_aircraft
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
5,000 lb
|
|
gptkbp:notable_features
|
spacious cabin
good performance
reliable engines
twin engine safety
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:payload_capacity
|
1,500 lb
|
|
gptkbp:primary_use
|
general aviation
|
|
gptkbp:production_years
|
1960-1982
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:related_aircraft
|
gptkb:Piper_Seminole
gptkb:Piper_Navajo
gptkb:Piper_Aztec_PA-23-150
gptkb:Piper_Aztec_PA-23-250
gptkb:Piper_Chieftain
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:stall_speed
|
70 knots
|
|
gptkbp:successor
|
gptkb:Piper_Navajo
|
|
gptkbp:type
|
twin-engine aircraft
|
|
gptkbp:variant
|
PA-23-150
PA-23-250
PA-23-260
|
|
gptkbp:wingspan
|
38 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Piper_Aztec_PA-23-260
|
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gptkbp:bfsLayer
|
7
|