Canadair CL-44 / CC-106 - Yukon
Data for (Version) | Canadair CL-44D-4 | |
First Flight | 15.11.1959 | |
Production Status | out of production | |
Production Range | 1960 - 1965 | |
Total Production | 39 | |
hull-loss occurrences | 21 | |
Developed from | Bristol Britannia | |
ICAO Code | CL44 CL4G | |
IATA Code | CL4 | |
Variants |
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ENGINE | 4 x Rolls-Royce Tyne 515/10, 4273kW | |
WEIGHTS | ||
Take-off weight | 95,254 kg | 210,000 lb |
Empty weight | 40,348 kg | 88,953 lb |
Internal fuel | kg 36944 | |
DIMENSIONS | ||
Wingspan | 43.37 m | 142 ft 3 in |
Length | 41.73 m | 137 ft 11 in |
Height | 11.18-11.79 m | 39 ft 8 in |
Wing area | 192.77 m2 | 2074.96 sq ft |
PERFORMANCE | ||
Cruise speed | 621-646 km/h | 386 mph |
Ceiling | 9145 m | 30000 ft |
Range w/max.fuel | 8990-8991 km | 5587 miles |
Range w/max.payload | 3798-4627 km | 2875 miles |
CREW | 3-4 | |
PASSENGERS | 214 | |
Payload |
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