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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Fairchild_PT-26_Cornell
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gptkbp:aircraft_operated
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gptkb:Fairchild_PT-19
gptkb:item
low-wing
civilian trainer
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
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|
gptkbp:cockpit
|
open cockpit
|
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gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:drivetrain
|
tailwheel landing gear
|
|
gptkbp:engine
|
gptkb:musical
|
|
gptkbp:engine_type
|
gptkb:Wright_R-975
gptkb:engine
|
|
gptkbp:first_flight
|
gptkb:1940
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.74 m
|
|
gptkbp:historical_significance
|
used for pilot training during WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PT-26 A
|
|
gptkbp:introduced
|
1941
|
|
gptkbp:is_used_by
|
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Canadian_Car_and_Foundry
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
250 m
1,600 kg
|
|
gptkbp:nickname
|
gptkb:Cornell
|
|
gptkbp:notable_features
|
good visibility
|
|
gptkbp:number_built
|
approximately 1,000
|
|
gptkbp:power_output
|
450 hp
|
|
gptkbp:primary_user
|
gptkb:Native_American_tribe
|
|
gptkbp:production_location
|
gptkb:Native_American_tribe
|
|
gptkbp:production_years
|
1940-1945
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:seating_capacity
|
400 kg
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:service_history
|
used in training and civilian roles
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:de_Havilland_Canada_DHC-1_Chipmunk
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
gptkb:PT-26
|
|
gptkbp:weight
|
1,200 kg
1,600 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.67 m
|