Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:tiltwing_aircraft
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:crew |
2
|
| gptkbp:engineType |
turboprop
|
| gptkbp:firstFlight |
1965
|
| gptkbp:length |
12.2 m
|
| gptkbp:manufacturer |
gptkb:Canadair
|
| gptkbp:maximumSpeed |
321 km/h
|
| gptkbp:nickname |
Dynavert
|
| gptkbp:numberBuilt |
4
|
| gptkbp:propulsion |
2 × Lycoming T53 turboshaft engines
|
| gptkbp:role |
experimental VTOL aircraft
|
| gptkbp:status |
retired
|
| gptkbp:survivesIn |
gptkb:Canada_Aviation_and_Space_Museum
|
| gptkbp:testOperators |
gptkb:Royal_Air_Force
gptkb:United_States_Army gptkb:United_States_Navy gptkb:Royal_Canadian_Air_Force |
| gptkbp:verticalTakeoffAndLanding |
yes
|
| gptkbp:wingspan |
14.6 m
|
| gptkbp:bfsParent |
gptkb:Western_Canada_Aviation_Museum
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Canadair CL-84 Dynavert
|