CANADAIR CL-415 Civil Aircraft Model Details

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General Information of CANADAIR CL-415

Developed From : Canadair CL-215

First Flight : 34309

Introduction : 1994

Manufacturer : Canadair (Canada One Plant - Saint-Laurent, Quebec (1960s-1980s) ; Bombardier Aerospace - Dorval; Quebec (1980s-present) and North Bay; Ontario (final assembly 1999-present)

Number Built : 88[2]

Primary Users : Canada; Italy; France; Greece; [1]

Role : Amphibious water bomber

Status : Active service

Unit_Cost : $32 million CAD [3]

General characteristics of CANADAIR CL-415

Airfoil : NACA 4417

Crew : 2 pilots

Empty Weight : 28,400 lb (12,880 kg)

Height : 29 ft 3 in (8.9 m)

Length : 65 ft (19.82 m)

Maximum Landing Weight : 37,000 lb (16,780 kg)

Payload : 6,400lb (2,900 kg)

Powerplant : 2 × Pratt & Whitney Canada PW123AF turboprop, takeoff power : 2,380 shp (1,775 kW) each

Wing Area : 1,080 sq ft (100 sq m)

Wingspan : 93 ft 11 in (28.6 m)

Performance of CANADAIR CL-415

Cruise Speed : 207 mph (333 km/h (180 kt))

Maximum Speed : 223 mph (359 km/h (194 kt))

Range : 1,518 miles (2,443 km)

Rate Of Climb : 1,600 ft/min (8.1 m/s)

Service Ceiling : 14,700 ft (4,500 m)

Stall Speed : 78 mph (126 km/h (68 kt))

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