Attribute | ![]() Canadair CL-44 × | ![]() Douglas DC-6 × |
---|---|---|
General | ||
Manufacturer | Bombardier Aerospace | Douglas Aircraft Co. |
Model | Canadair CL-44 | Douglas DC-6 |
Country | Canada | United States |
Manufactured from (year) | 1960 | 1946 |
Manufactured to (year) | 1965 | 1958 |
Type | Cargo Airplanes | Passenger Turbo Props |
Icao | CL44 | DC6 |
Performance | ||
Engine | 4x Rolls-Royce Tyne 515/50 | 4x Pratt & Whitney R-2800-CA15 "Double Wasp" |
Power, hp (hp) | 5,730 | 2,400 |
Max cruise speed (km/h) | 667 | 500 |
Approach speed (km/h) | - | 156 |
Travel range (km) | 8,993 | 4,811 |
Service ceiling (m) | 9,144 | 7,620 |
Rate of climb (m/sec) | - | 5.44 |
Take off distance (m) | - | 1,800 |
Landing distance (m) | - | 1,200 |
Weights | ||
Max take off weight (kg) | 95,000 | 44,100 |
Max payload (kg) | 30,000 | 12,700 |
Fuel tank capacity (l) | 37,002 | 17,875 |
Baggage volume (m³) | 28.3 | 15.1 |
Dimensions | ||
Seats | 189 | 68 |
Cabin height (m) | 2.05 | 2.1 |
Cabin width (m) | 3.35 | 3 |
Cabin length (m) | 30 | - |
Exterior length (m) | 41.7 | 30.6 |
Tail height (m) | 11.18 | 8.6 |
Fuselage diameter (m) | 3.7 | 3.1 |
Wing span (m) | 43.37 | 35.8 |
Wing tips | No Winglets | No Winglets |