Attribute | Value |
---|---|
General | |
Manufacturer | McDonnell Douglas |
Model | McDonnell Douglas C-9 Nightingale |
Country | United States |
Manufactured from | 1968 year |
Manufactured to | 1982 year |
Type | Military Aircraft |
Icao | DC9 |
Performance | |
Engine | 2x Pratt & Whitney JT8D-9 |
Power, hp | Add |
Power, lbf | 14,500 lbf |
Avionics | Add |
Max cruise speed | 926 km/h |
Approach speed | 235 km/h |
Travel range | 3,221 km |
Fuel economy | Add |
Service ceiling | 11,278 m |
Rate of climb | 15.24 m/sec |
Take off distance | 2,100 m |
Landing distance | 1,500 m |
Weights | |
Max take off weight | 50,000 kg |
Max landing weight | 44,906 kg |
Max payload | 13,674 kg |
Fuel tank capacity | 13,926 l |
Baggage volume | 25.3 m³ |
Dimensions | |
Seats | 84 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | 2.05 m |
Cabin width | 2.66 m |
Cabin length | Add |
Exterior length | 36.36 m |
Tail height | 8.5 m |
Fuselage diameter | 3.3 m |
Wing span | 28.44 m |
Wing tips | No Winglets |