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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:aircraft_operated
|
low-wing monoplane
military trainer
cantilever wing
twin-engine aircraft
trainer and bomber
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|
gptkbp:armament
|
machine guns
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|
gptkbp:cockpit
|
closed cockpit
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|
gptkbp:crew
|
2
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gptkbp:decommissioned
|
1960s
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gptkbp:design
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gptkb:Geoffrey_de_Havilland
gptkb:Airspeed_Ltd
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|
gptkbp:engine
|
2
450 hp
Armstrong Siddeley Cheetah
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|
gptkbp:engine_type
|
inline engine
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gptkbp:first_flight
|
1937
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gptkbp:fuel_capacity
|
1,200 L
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gptkbp:height
|
3.81 m
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gptkbp:historical_significance
|
training pilots during WWII
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Airspeed Oxford Mk II
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gptkbp:is_used_by
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gptkb:military_base
|
|
gptkbp:landing_gear
|
tailwheel
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|
gptkbp:length
|
11.43 m
|
|
gptkbp:manufacturer
|
gptkb:Airspeed_Ltd
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|
gptkbp:material
|
metal construction
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|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
90 km/h
3,175 kg
|
|
gptkbp:number_built
|
approximately 8,000
|
|
gptkbp:primary_user
|
gptkb:military_base
|
|
gptkbp:produced_by
|
gptkb:aircraft
|
|
gptkbp:production_years
|
1937-1943
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|
gptkbp:propulsion
|
2
|
|
gptkbp:range
|
1,600 km
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
1,000 kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
1939
|
|
gptkbp:speed
|
300 km/h
|
|
gptkbp:successor
|
gptkb:Airspeed_Ambassador
|
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gptkbp:used_in
|
gptkb:World_War_II
|
|
gptkbp:variant
|
gptkb:Airspeed_Oxford_Mk_I
|
|
gptkbp:wing_area
|
36.5 m²
|
|
gptkbp:wingspan
|
15.85 m
|
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gptkbp:bfsParent
|
gptkb:Airspeed_Oxford
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gptkbp:bfsLayer
|
7
|