Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:DHC-35_Dash_35
|
| gptkbp:avionics |
modern navigation systems
|
| gptkbp:cockpit |
pressurized
|
| gptkbp:crew |
1 pilot
|
| gptkbp:engine_type |
turboprop
|
| gptkbp:features |
high-wing configuration
|
| gptkbp:first_flight |
gptkb:1955
|
| gptkbp:fuel_capacity |
1,200 liters
|
| https://www.w3.org/2000/01/rdf-schema#label |
DHC-35-100
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
11.58 m
|
| gptkbp:manufacturer |
gptkb:De_Havilland_Canada
|
| gptkbp:max_takeoff_weight |
3,175 kg
|
| gptkbp:number_built |
approximately 200
|
| gptkbp:operational_history |
used in various roles including cargo and passenger transport.
|
| gptkbp:primary_user |
gptkb:aircraft
|
| gptkbp:production_years |
1955-1960
|
| gptkbp:range |
1,200 nautical miles
|
| gptkbp:role |
utility aircraft
|
| gptkbp:seating_capacity |
up to 6 passengers
|
| gptkbp:service_ceiling |
25,000 ft
|
| gptkbp:speed |
250 knots
|
| gptkbp:variant |
gptkb:DHC-35-200
|
| gptkbp:wingspan |
15.85 m
|