gptkbp:instance_of
|
gptkb:aircraft
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Piper_PA-30
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gptkbp:aircraft_operated
|
gptkb:aircraft
2,200 lbs
8 ft 6 in
170 knots
utility aircraft
low-wing
civil aircraft
26 ft 10 in
twin engines
3,800 lbs max takeoff weight
|
gptkbp:climb_rate
|
1,200 ft/min
|
gptkbp:cockpit
|
pressurized cockpit
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gptkbp:design
|
Piper Aircraft design team
|
gptkbp:engine
|
2
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gptkbp:engine_type
|
gptkb:Lycoming_IO-360
piston engine
|
gptkbp:first_flight
|
gptkb:1961
|
gptkbp:fuel_capacity
|
60 US gallons
|
gptkbp:height
|
8 ft 6 in
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-30 B
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
26 ft 10 in
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
gptkbp:market_segment
|
private and business aviation
|
gptkbp:marketed_as
|
gptkb:Piper_Twin_Comanche
|
gptkbp:max_speed
|
200 knots
|
gptkbp:max_takeoff_weight
|
3,800 lbs
|
gptkbp:notable_features
|
twin engines
|
gptkbp:origin
|
gptkb:United_States
|
gptkbp:produced_by
|
1,500 units
|
gptkbp:production_years
|
1961 to 1972
|
gptkbp:propulsion
|
constant-speed propellers
|
gptkbp:range
|
1,200 miles
1,200 nautical miles
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
4 to 6 passengers
|
gptkbp:service_ceiling
|
18,000 ft
|
gptkbp:speed
|
170 knots
60 knots
|
gptkbp:successor
|
gptkb:Piper_PA-34_Seneca
|
gptkbp:type
|
twin-engine aircraft
|
gptkbp:uses
|
general aviation
|
gptkbp:variant
|
gptkb:Piper_PA-30
gptkb:Piper_PA-39
|
gptkbp:weight
|
2,200 lbs
|
gptkbp:wingspan
|
38 ft 0 in
|