McDonnell Douglas DC-9-10 [+]Compare [E]dit [H]istory

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Object «McDonnell Douglas DC-9-10» has attributes

Attribute Value
General
Manufacturer Douglas Aircraft Co.
Model McDonnell Douglas DC-9-10
Country United States
Manufactured from 1965 year
Manufactured to 1969 year
Type Light Passenger Jets
Icao DC91
Performance
Engine 2x Pratt & Whitney JT8D-7
Power, hp Add
Power, lbf 14,000 lbf
Avionics Add
Max cruise speed 896 km/h
Approach speed 244 km/h
Travel range 2,685 km
Fuel economy Add
Service ceiling 10,668 m
Rate of climb 14.22 m/sec
Take off distance 1,615 m
Landing distance 1,320 m
Weights
Max take off weight 41,100 kg
Max landing weight 37,100 kg
Max payload 18,000 kg
Fuel tank capacity 13,979 l
Baggage volume 17 m³
Dimensions
Seats 9
Seats - business class Add
Seats - first class Add
Cabin height 2.1 m
Cabin width 3.1 m
Cabin length 18.29 m
Exterior length 31.82 m
Tail height 8.38 m
Fuselage diameter 3.34 m
Wing span 27.25 m
Wing tips No Winglets

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (45 fields were changed)
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