Douglas C-124 Globemaster II [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Douglas Aircraft Co. |
| Model | Douglas C-124 Globemaster II |
| Country | United States |
| Manufactured from | 1949 year |
| Manufactured to | 1955 year |
| Type | Military Transport Planes |
| Icao | C124 |
| Performance | |
| Engine | 4x Pratt & Whitney R-4360-63A Wasp Major |
| Power, hp | 3,800 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 489 km/h |
| Approach speed | Add |
| Travel range | 6,482 km |
| Fuel economy | Add |
| Service ceiling | 7,010 m |
| Rate of climb | 3.86 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights | |
| Max take off weight | 88,224 kg |
| Max landing weight | 88,224 kg |
| Max payload | 34,000 kg |
| Fuel tank capacity | 42,124 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 7 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | 23 m |
| Exterior length | 39.8 m |
| Tail height | 14.74 m |
| Fuselage diameter | 4.5 m |
| Wing span | 53.06 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (39 fields were changed)
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