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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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single-engine
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gptkbp:aircraft_operated
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gptkb:trainer_aircraft
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gptkbp:aircraft_type
|
military trainer
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|
gptkbp:armament
|
gptkb:none
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gptkbp:avionics
|
glass cockpit
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gptkbp:cockpit
|
side-by-side seating
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gptkbp:crew
|
2
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gptkbp:customer_support
|
gptkb:Royal_Air_Force
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gptkbp:design
|
low-wing monoplane
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gptkbp:design_feature
|
low maintenance costs
highly maneuverable
multi-role capabilities
advanced simulation capabilities
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gptkbp:engine_type
|
turboprop
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gptkbp:first_flight
|
gptkb:2007
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gptkbp:fuel_capacity
|
1,200 liters
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gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PC-21 Mk II
|
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
12.7 m
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gptkbp:manufacturer
|
gptkb:Pilatus_Aircraft
|
|
gptkbp:material
|
used in construction
|
|
gptkbp:max_speed
|
400 knots
|
|
gptkbp:max_takeoff_weight
|
2,800 kg
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:origin
|
gptkb:Switzerland
|
|
gptkbp:power_output
|
1,600 shp
|
|
gptkbp:production_status
|
in production
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|
gptkbp:provides_training_for
|
advanced flight training
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|
gptkbp:range
|
1,500 km
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
60 degrees per second
|
|
gptkbp:seating_capacity
|
yes
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:services
|
gptkb:Australia
gptkb:Saudi_Arabia
gptkb:Singapore
gptkb:Switzerland
gptkb:United_Arab_Emirates
|
|
gptkbp:simulator_availability
|
yes
|
|
gptkbp:stall_speed
|
75 knots
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:training_programs
|
integrated training system
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
10.7 m
|
|
gptkbp:bfsParent
|
gptkb:PC-21
|
|
gptkbp:bfsLayer
|
7
|