Comparison of Canadair CL-44 and Douglas C-133 Cargomaster [S]ave
| Attribute |  Douglas C-133 Cargomaster × |  Canadair CL-44 × |
|---|---|---|
| General | ||
| Manufacturer | Douglas Aircraft Co. | Bombardier Aerospace |
| Model | Douglas C-133 Cargomaster | Canadair CL-44 |
| Country | United States | Canada |
| Manufactured from (year) | 1956 | 1960 |
| Manufactured to (year) | 1961 | 1965 |
| Type | Military Transport Planes | Cargo Airplanes |
| Icao | C133 | CL44 |
| Performance | ||
| Engine | 4x Pratt & Whitney T34-P-9W | 4x Rolls-Royce Tyne 515/50 |
| Power, hp (hp) | 7,500 | 5,730 |
| Max cruise speed (km/h) | 578 | 667 |
| Travel range (km) | 6,593 | 8,993 |
| Service ceiling (m) | 9,129 | 9,144 |
| Rate of climb (m/sec) | 6.5 | - |
| Weights | ||
| Max take off weight (kg) | 129,727 | 95,000 |
| Max payload (kg) | 50,000 | 30,000 |
| Fuel tank capacity (l) | 69,031 | 37,002 |
| Baggage volume (m³) | - | 28.3 |
| Dimensions | ||
| Seats | 5 | 189 |
| Cabin height (m) | 3.7 | 2.05 |
| Cabin width (m) | 3.6 | 3.35 |
| Cabin length (m) | 27 | 30 |
| Exterior length (m) | 48 | 41.7 |
| Tail height (m) | 14.7 | 11.18 |
| Fuselage diameter (m) | 4.4 | 3.7 |
| Wing span (m) | 54.8 | 43.37 |
| Wing tips | No Winglets | No Winglets |
Help · Contact us · Disclaimer · Contributors · Developers · Donate