Comparison of Canadair CL-44 and Douglas C-74 Globemaster [S]ave
| Attribute |  Canadair CL-44 × |  Douglas C-74 Globemaster × |
|---|---|---|
| General | ||
| Manufacturer | Bombardier Aerospace | Douglas Aircraft Co. |
| Model | Canadair CL-44 | Douglas C-74 Globemaster |
| Country | Canada | United States |
| Manufactured from (year) | 1960 | 1945 |
| Manufactured to (year) | 1965 | 1947 |
| Type | Cargo Airplanes | Military Transport Planes |
| Icao | CL44 | C74 |
| Performance | ||
| Engine | 4x Rolls-Royce Tyne 515/50 | 4x Pratt & Whitney R-4360-69 Wasp Major |
| Power, hp (hp) | 5,730 | 3,250 |
| Max cruise speed (km/h) | 667 | 528 |
| Travel range (km) | 8,993 | 5,556 |
| Service ceiling (m) | 9,144 | 6,492 |
| Rate of climb (m/sec) | - | 13.23 |
| Weights | ||
| Max take off weight (kg) | 95,000 | 78,000 |
| Max payload (kg) | 30,000 | 21,840 |
| Fuel tank capacity (l) | 37,002 | 41,639 |
| Baggage volume (m³) | 28.3 | - |
| Dimensions | ||
| Seats | 189 | 13 |
| Cabin height (m) | 2.05 | - |
| Cabin width (m) | 3.35 | - |
| Cabin length (m) | 30 | - |
| Exterior length (m) | 41.7 | 37.8 |
| Tail height (m) | 11.18 | 13.34 |
| Fuselage diameter (m) | 3.7 | 4.1 |
| Wing span (m) | 43.37 | 52.8 |
| Wing tips | No Winglets | No Winglets |
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