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/ Comparison of McDonnell Douglas DC-9-10 and Bombardier CS300
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Comparison of McDonnell Douglas DC-9-10 and Bombardier CS300
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Attribute
Bombardier CS300
×
McDonnell Douglas DC-9-10
×
General
Manufacturer
Bombardier Aerospace
Douglas Aircraft Co.
Model
Bombardier CS300
McDonnell Douglas DC-9-10
Country
Canada
United States
Manufactured from (year)
2013
1965
Manufactured to (year)
-
1969
Type
Mid Size Passenger Jets
Light Passenger Jets
Icao
BCS3
DC91
Performance
Engine
2x Pratt And Whitney PW1500G
2x Pratt & Whitney JT8D-7
Power, lbf (lbf)
23,300
14,000
Avionics
Rockwell Collins Pro Line Fusion
-
Max cruise speed (km/h)
870
896
Approach speed (km/h)
259
244
Travel range (km)
6,112
2,685
Fuel economy (km/l)
0.396
-
Service ceiling (m)
12,497
10,668
Rate of climb (m/sec)
15.75
14.22
Take off distance (m)
1,890
1,615
Landing distance (m)
1,509
1,320
Weights
Max take off weight (kg)
67,585
41,100
Max landing weight (kg)
58,740
37,100
Max payload (kg)
18,711
18,000
Fuel tank capacity (l)
21,505
13,979
Baggage volume (m³)
31.6
17
Dimensions
Seats
16
9
Seats - business class
12
-
Cabin height (m)
2.1
2.1
Cabin width (m)
3.28
3.1
Cabin length (m)
27.5
18.29
Exterior length (m)
38.7
31.82
Tail height (m)
11.5
8.38
Fuselage diameter (m)
3.7
3.34
Wing span (m)
35.1
27.25
Wing tips
Blended Tips
No Winglets
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