Comparison of ATR 42-600 and Canadair CL-44 [S]ave
| Attribute |  Canadair CL-44 × |  ATR 42-600 × |
|---|---|---|
| General | ||
| Manufacturer | Bombardier Aerospace | ATR Aircraft |
| Model | Canadair CL-44 | ATR 42-600 |
| Country | Canada | France |
| Manufactured from (year) | 1960 | 2010 |
| Manufactured to (year) | 1965 | - |
| Type | Cargo Airplanes | Passenger Turbo Props |
| Icao | CL44 | - |
| Performance | ||
| Engine | 4x Rolls-Royce Tyne 515/50 | 2 X Pratt And Whitney PW 127M - |
| Power, hp (hp) | 5,730 | 2,160 |
| Avionics | - | Thales Avionics Suite Glass Cockpit |
| Max cruise speed (km/h) | 667 | 556 |
| Travel range (km) | 8,993 | 1,326 |
| Fuel economy (km/l) | - | 0.758 |
| Service ceiling (m) | 9,144 | - |
| Take off distance (m) | - | 1,036 |
| Landing distance (m) | - | 884 |
| Weights | ||
| Max take off weight (kg) | 95,000 | 18,600 |
| Max payload (kg) | 30,000 | 5,450 |
| Fuel tank capacity (l) | 37,002 | 4,497 |
| Baggage volume (m³) | 28.3 | - |
| Dimensions | ||
| Seats | 189 | 48 |
| Cabin height (m) | 2.05 | - |
| Cabin width (m) | 3.35 | - |
| Cabin length (m) | 30 | - |
| Exterior length (m) | 41.7 | 22.67 |
| Tail height (m) | 11.18 | - |
| Fuselage diameter (m) | 3.7 | - |
| Wing span (m) | 43.37 | 24.57 |
| Wing tips | No Winglets | No Winglets |
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