|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:De_Havilland_DH.60_Moth
|
|
gptkbp:aircraft_operated
|
gptkb:item
general aviation
|
|
gptkbp:capacity
|
6 passengers
|
|
gptkbp:cockpit
|
enclosed
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:R._J._Mitchell
|
|
gptkbp:engine
|
gptkb:musical
200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1946
1946-07-01
|
|
gptkbp:fuel_capacity
|
200 liters
|
|
gptkbp:height
|
3.05 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
De Havilland DH.93
|
|
gptkbp:introduced
|
1947
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
10.67 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
70 km/h
400 m
|
|
gptkbp:notable_features
|
easy handling
good visibility
high wing
stable flight characteristics
low drag design
|
|
gptkbp:number_built
|
50
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:primary_user
|
gptkb:military_base
|
|
gptkbp:production_years
|
1946-1950
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:role
|
passenger transport
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:successor
|
gptkb:De_Havilland_DH.94
|
|
gptkbp:surface
|
gptkb:public_transportation_system
rudder
aileron
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
DH.93 A
DH.93 B
|
|
gptkbp:wing_area
|
30.5 m²
|
|
gptkbp:wingspan
|
15.24 m
|