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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Alfred_A._De_Havilland
gptkb:Hugh_A._De_Havilland
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gptkbp:crew
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gptkb:3
2
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gptkbp:design
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gptkb:Sir_Geoffrey_de_Havilland
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gptkbp:engine
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gptkb:3
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gptkbp:engine_type
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gptkb:Rolls-Royce_RB.163
turbofan
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gptkbp:features
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gptkb:military_base
advanced avionics
high fuel efficiency
quiet operation
high-wing configuration
large cargo hold
modern cabin design
short takeoff and landing capability
emergency exit doors
low drag design
three-engine configuration
large passenger windows
comfortable seating arrangement
rear fuselage mounted engines
t-tail configuration
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gptkbp:first_flight
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2004-01-01
1964-04-01
1962-01-09
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gptkbp:fuel_capacity
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12,000 liters
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gptkbp:height
|
10.5 m
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|
https://www.w3.org/2000/01/rdf-schema#label
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De Havilland DH.121 Trident
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gptkbp:introduced
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gptkb:1964
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gptkbp:length
|
38.4 m
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gptkbp:manufacturer
|
gptkb:De_Havilland
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gptkbp:max_speed
|
850 km/h
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|
gptkbp:max_takeoff_weight
|
60,000 kg
55,000 kg
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|
gptkbp:notable_event
|
1972 Trident crash
1980 Dan-Air Trident crash
1985 Trident crash
1990 Trident incident
1994 Trident incident
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gptkbp:number_built
|
117
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gptkbp:primary_user
|
gptkb:Bristol_Britannia
gptkb:Dan-Air
gptkb:British_Airways
gptkb:Air_Malta
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|
gptkbp:range
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3,000 km
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gptkbp:retired
|
gptkb:2004
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|
gptkbp:seating_capacity
|
180
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gptkbp:services
|
gptkb:1964
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gptkbp:status
|
retired
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gptkbp:variant
|
gptkb:Trident_1
gptkb:Trident_2
gptkb:Trident_3
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gptkbp:wing_area
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200 m²
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gptkbp:wingspan
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34.3 m
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