Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:DHC-26_Dash_26
|
| gptkbp:crew |
2
|
| gptkbp:design |
short takeoff and landing (STOL)
|
| gptkbp:engine_type |
piston engine
|
| gptkbp:first_flight |
gptkb:1956
|
| gptkbp:height |
3.66 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
DHC-26 C
|
| gptkbp:length |
10.67 m
|
| gptkbp:manufacturer |
gptkb:De_Havilland_Canada
|
| gptkbp:max_speed |
250 km/h
|
| gptkbp:max_takeoff_weight |
3,402 kg
|
| gptkbp:number_built |
approximately 100
|
| gptkbp:primary_user |
gptkb:military_unit
|
| gptkbp:production_years |
1956-1960
|
| gptkbp:range |
1,500 km
|
| gptkbp:role |
utility aircraft
|
| gptkbp:seating_capacity |
gptkb:6
|
| gptkbp:service_ceiling |
3,000 m
|
| gptkbp:variant |
gptkb:DHC-6_Twin_Otter
|
| gptkbp:wing_area |
30.5 m²
|
| gptkbp:wingspan |
14.63 m
|