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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
|
twin-engine piston
|
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gptkbp:aircraft_operated
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gptkb:light_aircraft
|
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gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:climb_rate
|
1,200 ft/min
|
|
gptkbp:cockpit
|
pressurized
|
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gptkbp:crew
|
gptkb:1
|
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gptkbp:design
|
utility aircraft
Piper Aircraft engineers
|
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gptkbp:engine_type
|
gptkb:Lycoming_IO-540
|
|
gptkbp:first_flight
|
gptkb:1966
|
|
gptkbp:flaps
|
split flaps
|
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gptkbp:fuel_capacity
|
120 gallons
|
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gptkbp:fuel_type
|
avgas
|
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gptkbp:fuselage_material
|
all-metal construction
|
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gptkbp:height
|
8 ft 10 in
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-31-300 Navajo
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gptkbp:landing_gear
|
retractable
tricycle gear
|
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gptkbp:length
|
28 ft 9 in
|
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gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:max_speed
|
200 knots
|
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gptkbp:max_takeoff_weight
|
5,000 lbs
|
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gptkbp:notable_users
|
gptkb:Royal_Air_Force
gptkb:United_States_Air_Force
Various charter airlines
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gptkbp:number_of_engines
|
2
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gptkbp:orbital_altitude
|
10,000 ft
|
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gptkbp:passenger_capacity
|
gptkb:6
|
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gptkbp:power_output
|
300 hp
|
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gptkbp:produces
|
1,200 units
|
|
gptkbp:production_years
|
1966-1984
|
|
gptkbp:propeller
|
constant speed
|
|
gptkbp:range
|
1,200 nautical miles
|
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gptkbp:role
|
light transport aircraft
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:successor
|
gptkb:Piper_PA-31_T_Cheyenne
|
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gptkbp:tail_type
|
T-tail
|
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gptkbp:type
|
twin-engine
|
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gptkbp:variant
|
Piper PA-31-325 Navajo Chieftain
|
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gptkbp:weight
|
3,200 lbs
|
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gptkbp:wing_configuration
|
low-wing
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gptkbp:wingspan
|
39 ft 6 in
|
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gptkbp:bfsParent
|
gptkb:Piper_PA-31_Navajo
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gptkbp:bfsLayer
|
5
|