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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:de_Havilland_Venom
|
|
gptkbp:aircraft_operated
|
gptkb:de_Havilland_Heron
gptkb:de_Havilland_Dragon_Rapide
gptkb:de_Havilland_Tiger_Moth
gptkb:de_Havilland_Hornet_Moth
gptkb:de_Havilland_Dove
cantilever wing
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:R._J._Mitchell
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
all-metal construction
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:first_introduced
|
1948
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
1,500 liters
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
de Havilland Albatross
|
|
gptkbp:influenced_by
|
gptkb:de_Havilland_Comet
gptkb:de_Havilland_Mosquito
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
19.81 m
|
|
gptkbp:manufacturer
|
gptkb:de_Havilland
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
5,670 kg
|
|
gptkbp:notable_users
|
gptkb:Australian_National_Airways
gptkb:Trans_Australia_Airlines
gptkb:New_Zealand_National_Airways_Corporation
gptkb:military_base
|
|
gptkbp:produced_by
|
50
|
|
gptkbp:production_years
|
1947-1950
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
1,500 kg
up to 14
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:surface
|
elevators
ailerons
rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
de Havilland Albatross Mk I
de Havilland Albatross Mk II
|
|
gptkbp:wingspan
|
28.96 m
|