McDonnell Douglas C-9 Nightingale [+]Compare [E]dit [H]istory

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Object «McDonnell Douglas C-9 Nightingale» has attributes

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

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (44 fields were changed)
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