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McDonnell Douglas C-9A


General information


ManufacturerMcDonnell Douglas
ModelC-9 Nightingale
ModificationC-9A
CountryUSA
Years1963
TypeTransport aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan28.47 m
Length36.37 m
Height8.38 m
Wing area92.97 m2
Zero fuel weight-
Empty weight25940 kg
Maximum takeoff weight54885 kg
Normal takeoff weight-
Flight duration-
Engine2 Pratt Whitney JT8D-9
Power-
Thrust2 x 64.50 kN
Maximum speed995 km/h
Cruising speed907 km/h
Rate of climb-
Practical range3669 km
Service ceiling11280 m
Hovering ceiling-
Crew2-3