Douglas DC-9. A photo. Video. Driving compartment. Characteristics. Reviews.
The McDonnell Douglas DC9 (also known as the Douglas DC9) is a short-range twin-engine jet aircraft. In 1965, the first flight began to be carried out in 1966. The last DS9 was produced in October 1982.
Subsequent variations in DC-9 were MD80, MD90 and Boing717.
Aerodynamic configuration of the aircraft is a twin-engine turbofan nizkoplan with a T-tail, swept wing, adjustable stabilizer and rear mounted engine.
Characteristics Douglas DC-9:
DC9-10
Number of seats: 90mest.
Flight range: 2340km.
Cruising speed: 903km / h.
Length: 31.82m.
Height: 8.38m.
Wingspan: 27.25m.
Maximum takeoff weight: 41100 kg
Motor type: Pratt & Whitney JT8D5.
DC9-21
Number of seats: 90mest.
Flight range: 3430 km.
Cruising speed: 896km / h.
Length: 31.82m.
Height: 8.38m.
Wingspan: 28.47m.
Maximum takeoff weight: 41100 kg
Motor type: Pratt & Whitney JT8D5.
Douglas DC-9 scheme salon
DC9-30
Number of seats: 115mest.
Flight range: 3030km.
Cruising speed: 917 km / h.
Length: 36.37m.
Height: 8.38m.
Wingspan: 28.47m.
Maximum takeoff weight: 49900kg
Motor type: Pratt & Whitney JT8D15.
DC9-40
Number of seats: 125mest.
Flight range: 3120 km.
Cruising speed: 917 km / h.
Length: 38.28m.
Height: 8.38m.
Wingspan: 28.47m.
Maximum takeoff weight: 51700kg
Motor type: Pratt & Whitney JT8D15.
DC9-50
Number of seats: 135mest.
Flight range: 3030km.
Cruising speed: 898km / h.
Length: 40.72m.
Height: 8.38m.
Wingspan: 28.47m.
Maximum takeoff weight: 54900kg
Motor type: Pratt & Whitney JT8D17.
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