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Start | Douglas | DC-9-40



Douglas DC-9-40


General information


ManufacturerDouglas
ModelDC-9-40
ModificationDC-9-40
CountryUSA
Years1967
TypePassenger aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan28.50 m
Length38.30 m
Height8.50 m
Wing area93.00 m2
Zero fuel weight27800 kg
Empty weight-
Maximum takeoff weight-
Normal takeoff weight51700 kg
Flight duration-
Engine-
Power-
Thrust-
Maximum speed940 km/h
Cruising speed900 km/h
Rate of climb-
Practical range1050 km
Service ceiling10670 m
Hovering ceiling-
Crew2-3
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