Attribute | Value |
---|---|
General | |
Manufacturer | Douglas Aircraft Co. |
Model | Douglas A-1 Skyraider |
Country | United States |
Manufactured from | 1945 year |
Manufactured to | 1957 year |
Type | Military Propellor Planes |
Icao | A1 |
Performance | |
Engine | 1x Wright R-3350-26WA Duplex-Cyclone |
Power, hp | 2,700 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 519 km/h |
Approach speed | Add |
Travel range | 2,437 km |
Fuel economy | Add |
Service ceiling | 8,687 m |
Rate of climb | 14.48 m/sec |
Take off distance | 400 m |
Landing distance | 800 m |
Weights | |
Max take off weight | 11,340 kg |
Max landing weight | Add |
Max payload | 3,800 kg |
Fuel tank capacity | 1,438 l |
Baggage volume | Add |
Dimensions | |
Seats | 1 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 11.9 m |
Tail height | 4.78 m |
Fuselage diameter | 1.5 m |
Wing span | 15.24 m |
Wing tips | No Winglets |