Canadair CL-44

· CANADAIR · 4 × Rolls-Royce Tyne

Airplanes

Length

41.73 m

Flat Wing Span

43.37 m

Height

11.18 m

Flat Wing Area

192.7 m²

Max Seating

160

Cruise Speed

646 km/h

Max Speed

670 km/h

Max Ceiling

9144 m

Number of Engines

Aircraft Engine

First Flight

1959-11-16

Entry Into service

1960-07-19

Number Built

Maximum Take-Off Weight

95 t (paragliders: kg)

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Canadair CL-44	95

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Shanghai Y-10		42.93	42.24		Compare
Boeing 720	Pratt & Whitney J57	41.4528	39.624	137	Compare
Bristol Britannia		37.7952	43.2816	139	Compare
Short Belfast		41.4528	48.1584	150	Compare
Convair R3Y Tradewind		42.3672	44.196	80	Compare
Canadair CP-107 Argus		40.2336	43.2816		Compare

All data (24 fields)

Name: Canadair CL-44
Manufacturer: CANADAIR
Description: The Canadair CL-44 was a Canadian turboprop airliner and cargo aircraft based on the Bristol Britannia that was developed and produced by Canadair in the late 1950s and early 1960s.
First Flight: 1959-11-16
Entry Into service: 1960-07-19
Service End: 1971-01-01
Designer: CANADAIR
Type: Military transport aircraft, Cargo aircraft
Length (m): 41.73
Height (m): 11.18
Cockpit Crew: 2
Max Seating: 160
Max Speed (km/h): 670
Cruise Speed (km/h): 646
Max Ceiling (m): 9144
Capacity Description: 160 passengers and 66,048 lb (29,959 kg) useful load
Number Built: 39
Powerplant Description: 4 × Rolls-Royce Tyne 515/50 turboprops, 4270 kW (5726 hp) each
Primary Users: Royal Canadian Air Force, Various airlines
Wikipedia Article (URL): en.wikipedia.org/wiki/Canadair_CL-44
Flat Wing Span (m): 43.37
Flat Wing Area (m²): 192.7
Aircraft Engine: Rolls-Royce Tyne
Number of Engines: 4