Attribute | Value |
---|---|
General | |
Manufacturer | Douglas Aircraft Co. |
Model | McDonnell Douglas DC-9-10 |
Country | United States |
Manufactured from | 1965 year |
Manufactured to | 1969 year |
Type | Light Passenger Jets |
Icao | DC91 |
Performance | |
Engine | 2x Pratt & Whitney JT8D-7 |
Power, hp | Add |
Power, lbf | 14,000 lbf |
Avionics | Add |
Max cruise speed | 896 km/h |
Approach speed | 244 km/h |
Travel range | 2,685 km |
Fuel economy | Add |
Service ceiling | 10,668 m |
Rate of climb | 14.22 m/sec |
Take off distance | 1,615 m |
Landing distance | 1,320 m |
Weights | |
Max take off weight | 41,100 kg |
Max landing weight | 37,100 kg |
Max payload | 18,000 kg |
Fuel tank capacity | 13,979 l |
Baggage volume | 17 m³ |
Dimensions | |
Seats | 9 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | 2.1 m |
Cabin width | 3.1 m |
Cabin length | 18.29 m |
Exterior length | 31.82 m |
Tail height | 8.38 m |
Fuselage diameter | 3.34 m |
Wing span | 27.25 m |
Wing tips | No Winglets |