| 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 |