|
gptkbp:instanceOf
|
amphibious aircraft
|
|
gptkbp:aircraft
|
fixed-wing aircraft
twin-engine
high-wing
special mission aircraft
CL-215T, CL-215-1A10
|
|
gptkbp:armament
|
none
|
|
gptkbp:capacity
|
1,600 gallons of water
|
|
gptkbp:cockpit
|
two-seat cockpit
|
|
gptkbp:constructionMaterial
|
aluminum
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
various operators
|
|
gptkbp:design
|
high-wing monoplane
Canadair_engineers
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_Canada_PT6A-34
|
|
gptkbp:engineType
|
turboprop
|
|
gptkbp:firstFlight
|
1967
|
|
gptkbp:fuelCapacity
|
1,800 liters
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
5.8 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Canadair CL-215
|
|
gptkbp:influencedBy
|
Canadair CL-215T
|
|
gptkbp:landingGear
|
retractable
|
|
gptkbp:legacy
|
pioneered aerial firefighting techniques.
|
|
gptkbp:length
|
16.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Canadair
|
|
gptkbp:maximumDepth
|
1,500 kg
|
|
gptkbp:maxSpeed
|
190 knots
|
|
gptkbp:maxTakeoffWeight
|
5,600 kg
|
|
gptkbp:modifications
|
various firefighting modifications
|
|
gptkbp:notableUsers
|
Canada,_France,_Italy
|
|
gptkbp:numberBuilt
|
more than 125
|
|
gptkbp:operationalHistory
|
used in various firefighting missions
|
|
gptkbp:operationalRange
|
1,200 km
|
|
gptkbp:participatesIn
|
none
|
|
gptkbp:primaryFunction
|
aerial firefighting
|
|
gptkbp:productionLocation
|
gptkb:Montreal,_Canada
|
|
gptkbp:productionYears
|
1967-1990
|
|
gptkbp:range
|
1,200 kilometers
|
|
gptkbp:retired
|
various dates by different operators
|
|
gptkbp:retirementYear
|
age, maintenance costs
|
|
gptkbp:role
|
firefighting aircraft
|
|
gptkbp:services
|
1969
3,000 meters
|
|
gptkbp:successor
|
gptkb:Canadair_CL-415
|
|
gptkbp:takeoffDistance
|
1,200 meters
1,000 meters
|
|
gptkbp:usedBy
|
various firefighting agencies
|
|
gptkbp:waterQuality
|
6,140 liters
|
|
gptkbp:wingArea
|
60.5 m²
|
|
gptkbp:wingspan
|
20.3 meters
|