Canadair CL-215 / CL-415
Designed principally for firefighting duties, the CL-215 twin-engined general-purpose amphibian also has military applications, including search and rescue and coastal patrol, Spain and Thailand use their CL-215s in both of these roles. The first prototype flew on October 23, 1967.
Canadair offers a number of special military configurations, including flight inspection, maritime surveillance using an ALL AN/APS-128 search radar, electronic warfare support and training, cargo transport, and airborne early warning (AEW).
Production of the basic CL-215 was completed with delivery in 1990 of the 126th airframe, having been exported to France, Greece, Spain, Italy, Yugoslavia, Thailand and Venezuela.
In September 1986 Canadair announced the CL-215T turboprop development. Designed as a retrofit package for existing operators of the piston-engined aircraft and - if sufficient new orders were received - for full production, the CL-215T has two 2,380 shp (1 175 kW) PW123AF engines driving four-bladed propellers. As a water-bomber (its primary mission) the CL-215T will carry 6,132 litres (1,620 US gal).
Engines: 2 x Pratt & Whitney R-2800-CA3, 1566kW, 2100hp
Max Take-off weight: 17100-19731 kg / 37699 - 43500 lb
Empty weight: 12161 kg / 26811 lb
Wingspan: 28.6 m / 94 ft 10 in
Length: 19.82 m / 65 ft 0 in
Height: 8.92 m / 29 ft 3 in
Wing area: 100.33 sq.m / 1079.94 sq ft
Max level speed: 172 mph ( 293 kph)
Cruise speed: 291 km/h / 181 mph
Range: 2095 km / 1302 miles
Payload: 5455kg of water