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/ Comparison of Bombardier CS300 and McDonnell Douglas DC-9-30
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Comparison of Bombardier CS300 and McDonnell Douglas DC-9-30
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Attribute
Bombardier CS300
×
McDonnell Douglas DC-9-30
×
General
Manufacturer
Bombardier Aerospace
McDonnell Douglas
Model
Bombardier CS300
McDonnell Douglas DC-9-30
Country
Canada
United States
Manufactured from (year)
2013
1965
Manufactured to (year)
-
1982
Type
Mid Size Passenger Jets
Mid Size Passenger Jets
Icao
BCS3
DC93
Performance
Engine
2x Pratt And Whitney PW1500G
2x JT8D-11
Power, lbf (lbf)
23,300
15,000
Avionics
Rockwell Collins Pro Line Fusion
-
Max cruise speed (km/h)
870
898
Approach speed (km/h)
259
235
Travel range (km)
6,112
2,778
Fuel economy (km/l)
0.396
-
Service ceiling (m)
12,497
10,668
Rate of climb (m/sec)
15.75
10.16
Take off distance (m)
1,890
2,100
Landing distance (m)
1,509
1,500
Weights
Max take off weight (kg)
67,585
48,988
Max landing weight (kg)
58,740
44,906
Max payload (kg)
18,711
13,674
Fuel tank capacity (l)
21,505
13,926
Baggage volume (m³)
31.6
25.3
Dimensions
Seats
16
115
Seats - business class
12
-
Cabin height (m)
2.1
2.05
Cabin width (m)
3.28
3.12
Cabin length (m)
27.5
22.79
Exterior length (m)
38.7
36.36
Tail height (m)
11.5
8.5
Fuselage diameter (m)
3.7
3.35
Wing span (m)
35.1
28.44
Wing tips
Blended Tips
No Winglets
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