CANADAIR CL-44 Civil Aircraft Model Details

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General Information of CANADAIR CL-44

Developed From : Bristol Britannia

First Flight : 21870

Introduction : 19 July 1960 (RCAF)

Manufacturer : Canadair

Number Built : 39

Primary Users : Royal Canadian Air Force; Various airlines

Retired : 1971 (CAF)

Role : Military transport aircraft; Cargo aircraft

Variants : Conroy Skymonster

General characteristics of CANADAIR CL-44

Capacity : 160 passengers

Crew : 3 (4 including loadmaster)

Empty Weight : 88,952 lb (40,348 kg)

Height : 36 ft 8 in (11.18 m)

Length : 136 ft 11 in (41.73 m)

Max Takeoff Weight : 210,000 lb (95,000 kg)

Powerplant : 4 × Rolls-Royce Tyne 515/50 turboprops, 5,730 shp (4,270 kW) each

Propellers : Four-blade variable pitch propellers

Useful Load : 66,048 lb (29,959 kg)

Wing Area : 2,075 ft² (192.7 m²)

Wingspan : 142 ft 4 in (43.37 m)

Performance of CANADAIR CL-44

Cruise Speed : 349 knots (402 mph, 646 km/h)

Range : 4,855 nm (5,588 mi, 8,990 km)

Service Ceiling : 30,000 ft (9,100 m)

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