Canadair CL-415

Airplanes

Length

20.4 m

Flat Wing Span

28.3799 m

Height

9.0068 m

Flat Wing Area

100.3353 m²

Max Seating

Cruise Speed

333 km/h

Max Speed

359 km/h

Number of Engines

Aircraft Engine

First Flight

1993-12-06

Entry Into service

1994-01-01

Number Built

Maximum Take-Off Weight

19.89 t (paragliders: kg)

Total Fuel Capacity

5812

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
Canadair CL-415	19.89	5812

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Canadair CL-215	Pratt & Whitney R-2800 Double Wasp	19.82	28.6	26	Compare
Martin 4-0-4	Pratt & Whitney R-2800 Double Wasp	22.5552	28.3464	40	Compare
Vickers Warwick		21.9456	29.2608		Compare
Handley Page Dart Herald		22.86	28.6512	56	Compare
Sud-Ouest Bretagne		18.95	26.9	43	Compare
Martin 2-0-2		21.6408	28.3464	40	Compare

All data (28 fields)

Name: Canadair CL-415
Manufacturer: Bombardier
Description: The Canadair CL-415 (Super Scooper, later Bombardier 415) and the De Havilland Canadair DHC-515 are a series of amphibious aircraft built originally by Canadair and subsequently by Bombardier and De Havilland Canada.
ICAO Code: CL2T
First Flight: 1993-12-06
Entry Into service: 1994-01-01
Designer: Bombardier
Length (m): 20.4
Height (m): 9.0068
Cockpit Crew: 2
Max Seating: 18
Max Speed (km/h): 359
Cruise Speed (km/h): 333
Min Speed (km/h): 126
Rate of Climb (m/s): 5.9436
Capacity Description: 6137 L (waterbombing), up to 18 paratroops, up to 2903 kg of cargo
Endurance (h): 3
National Origin: Canada
Number Built: 95
Powerplant Description: 2 × Pratt & Whitney Canada PW123AF turboprop, 1775 kW (2380 hp) each
Primary Users: Vigili del Fuoco (Italy), Sécurité Civile (France), Hellenic Air Force (Greece), Service Aérien Gouvernemental
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Canadair_CL-415
Flat Wing Span (m): 28.3799
Flat Wing Area (m²): 100.3353
Wake Category: M
Aircraft Engine: Pratt & Whitney Canada PW100
Number of Engines: 2