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Canadair CL-415 ✕ Martin 2-0-2 ✕
Manufacturer Bombardier Glenn L. Martin Company
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. The Martin 2-0-2 was a low-wing, all-metal, twin piston-engined American airliner designed and built by the Glenn L.
ICAO Code CL2T
First Flight 1993-12-06 1946-11-22
Entry Into service 1994-01-01 1947-01-01
Production End 1948-01-01
Service End 1975-01-01
Designer Bombardier Glenn L. Martin Company
Type Airliner
Length (m) 20.4 21.6408
Height (m) 9.0068 8.5344
Cockpit Crew 2 2
Max Seating 18 40
Max Speed (km/h) 359 500.506
Cruise Speed (km/h) 333 471.5378
Min Speed (km/h) 126 122.3101
Max Ceiling (m) 10058.4
Rate of Climb (m/s) 5.9436 11.176
Capacity Description 6137 L (waterbombing), up to 18 paratroops, up to 2903 kg of cargo ; 40 passengers or; 9270 lb payload
Endurance (h) 3
National Origin Canada Canada
Number Built 95 47
Powerplant Description 2 × Pratt & Whitney Canada PW123AF turboprop, 1775 kW (2380 hp) each 2 × Pratt & Whitney R-2800 CA-18 Double Wasp 18-cylinder air-cooled radial engine, 1342 kW (1800 hp) each
Primary Users Vigili del Fuoco (Italy), Sécurité Civile (France), Hellenic Air Force (Greece), Service Aérien Gouvernemental Northwest Orient Airlines, LAN Chile , Trans World Airlines
Status In service Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Canadair_CL-415 en.wikipedia.org/wiki/Martin_2-0-2
Flat Wing Span (m) 28.3799 28.3464
Flat Wing Area (m²) 100.3353 80.2682
Wake Category M
Aircraft Engine Pratt & Whitney Canada PW100
Number of Engines 2 2