Manufacturer | McDonnell Douglas |
Model | C-9 Nightingale |
Modification | C-9A |
Country | USA |
Years | 1963 |
Type | Transport aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 28.47 m |
Length | 36.37 m |
Height | 8.38 m |
Wing area | 92.97 m2 |
Zero fuel weight | - |
Empty weight | 25940 kg |
Maximum takeoff weight | 54885 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 2 Pratt Whitney JT8D-9 |
Power | - |
Thrust | 2 x 64.50 kN |
Maximum speed | 995 km/h |
Cruising speed | 907 km/h |
Rate of climb | - |
Practical range | 3669 km |
Service ceiling | 11280 m |
Hovering ceiling | - |
Crew | 2-3 |