gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_configuration
|
low-wing monoplane
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gptkbp:aircraft_operated
|
2.5 m
8.4 m
300 km/h
10.8 m
20 m³
military trainer
|
gptkbp:aircraft_type
|
single-engine aircraft
|
gptkbp:armament
|
gptkb:none
|
gptkbp:aspect_ratio
|
7.2
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gptkbp:climb_rate
|
1,200 ft/min
6 m/s
|
gptkbp:cockpit
|
pressurized cockpit
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gptkbp:crew
|
gptkb:1
|
gptkbp:design
|
gptkb:Pilatus_Aircraft_Ltd.
basic trainer
|
gptkbp:engine_power
|
550 shp
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
gptkbp:first_flight
|
gptkb:1966
|
gptkbp:fuel_capacity
|
1,200 L
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pilatus PC-7
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.4 m
|
gptkbp:manufacturer
|
gptkb:Pilatus_Aircraft
|
gptkbp:max_speed
|
300 km/h
|
gptkbp:max_takeoff_weight
|
2,800 kg
|
gptkbp:notable_operators
|
gptkb:Swiss_Air_Force
|
gptkbp:number_built
|
over 600
|
gptkbp:operational_use
|
1970s
|
gptkbp:originated_in
|
PC-9
|
gptkbp:payload_capacity
|
1,000 kg
|
gptkbp:power_source
|
gptkb:PT6_A-25_A_engine
|
gptkbp:production_years
|
1966–present
|
gptkbp:propeller
|
four-blade propeller
|
gptkbp:provides_training_for
|
basic and advanced training
|
gptkbp:range
|
1,500 km
|
gptkbp:role
|
gptkb:trainer_aircraft
|
gptkbp:roll_rate
|
4.5°/s
|
gptkbp:service
|
1970s to present
|
gptkbp:service_ceiling
|
10,000 m
|
gptkbp:service_entry
|
gptkb:1970
|
gptkbp:stall_speed
|
85 km/h
|
gptkbp:training
|
pilot training
|
gptkbp:used_by
|
various air forces
|
gptkbp:variant
|
gptkb:PC-7_Mk_II
|
gptkbp:weight
|
1,600 kg
|
gptkbp:wing_area
|
15.5 m²
|
gptkbp:wingspan
|
10.8 m
|
gptkbp:bfsParent
|
gptkb:Paraguayan_Air_Force
gptkb:Austrian_Air_Force
gptkb:Uruguayan_Air_Force
gptkb:Oman_Royal_Air_Force
gptkb:Royal_Air_Force_of_Oman
gptkb:Oman_Air_Force
gptkb:Malaysia_Air_Force
gptkb:Dominican_Air_Force
gptkb:Senegalese_Air_Force
gptkb:Belgian_Air_Force
gptkb:Honduras_Air_Force
gptkb:Honduran_Air_Force
gptkb:Royal_Air_Force_of_Ethiopia
|
gptkbp:bfsLayer
|
5
|