CANADAIR CL-215 Civil Aircraft Model Details

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General Information of CANADAIR CL-215

First Flight : 24768

Introduction : 1969

Manufacturer : Canadair

Number Built : 125

Primary Users : Canada; Greece; Spain

Produced : 1969–1990

Role : Firefighting amphibious aircraft

Status : Active service.

Variants : Bombardier 415

General characteristics of CANADAIR CL-215

Capacity : 18 passengers (utility version)

Crew : two pilots

Empty Weight : 12,065 kg (26,600 lb)

Height : 8.98 m (29 ft 6 in[22])

Length : 19.82 m (65 ft 0½ in)

Max Takeoff Weight : From water: 17,100 kg (37,700 lb), From land: 19,730 kg (43,500 lb)

Payload : 5,346 litres (1,176 Imp gal) of water or 5,444 kg (12,000 lb) of chemicals

Powerplant : 2 × Pratt & Whitney R-2800-83AM 18-cylinder radial engines, 2,100 hp (1,566 kW) each

Wing Area : 100.3 m² (1,080 ft²)

Wingspan : 28.60 m (93 ft 10 in)

Performance of CANADAIR CL-215

Cruise Speed : 291 km/h (157 knots, 181 mph) (max recommended power)

Range : 2,260 km (1,220 nm, 1,405 mi)

Rate Of Climb : 5 m/s (1,000 ft/min)

Service Ceiling : 14,600 ft (4,450 m)

Stall Speed : 123 km/h (66 knots, 76 mph)

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