Canadair CL-215

Airplanes

Length

19.82 m

Flat Wing Span

28.6 m

Height

8.92 m

Flat Wing Area

100.33 m²

Flat Wing Aspect Ratio

8.15

Max Seating

Cruise Speed

291 km/h

Number of Engines

Aircraft Engine

First Flight

1967-10-23

Entry Into service

1969-01-01

Number Built

125

Maximum Take-Off Weight

19.731 t (paragliders: kg)

Total Fuel Capacity

5910

Maximum Range

2094 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Canadair CL-215	19.731	5910	2094

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Canadair CL-415	Pratt & Whitney Canada PW100	20.4	28.3799	18	Compare
Sud-Ouest Bretagne		18.95	26.9	43	Compare
North American XB-21	Pratt & Whitney R-2180-A Twin Hornet	18.5928	28.956		Compare
Handley Page Dart Herald		22.86	28.6512	56	Compare
Vickers Warwick		21.9456	29.2608		Compare
Douglas DC-3		19.7	29	32	Compare

All data (26 fields)

Name: Canadair CL-215
Manufacturer: Bombardier
Description: The Canadair CL-215 Scooper is the first model in a series of amphibious flying boats designed and built by Canadian aircraft manufacturer Canadair, and later produced by Bombardier.
ICAO Code: CL2P
First Flight: 1967-10-23
Entry Into service: 1969-01-01
Designer: Bombardier
Length (m): 19.82
Height (m): 8.92
Max Seating: 26
Cruise Speed (km/h): 291
Min Speed (km/h): 123
Rate of Climb (m/s): 5
Capacity Description: 5,450 L (1200 imp gal; 1,440 US gal)(waterbombing), up to 26 forward facing seats for passenger transport
National Origin: Canada
Number Built: 125
Powerplant Description: 2 × Pratt & Whitney R-2800-83AM 18-cylinder air-cooled radial piston engines, 1566 kW (2100 hp) each
Primary Users: Canada, Greece , Spain , United States
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Canadair_CL-215
Flat Wing Span (m): 28.6
Flat Wing Area (m²): 100.33
Flat Wing Aspect Ratio: 8.15
Wake Category: M
Aircraft Engine: Pratt & Whitney R-2800 Double Wasp
Number of Engines: 2