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/ Comparison of Bombardier CS300 and McDonnell Douglas C-9 Nightingale
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Comparison of Bombardier CS300 and McDonnell Douglas C-9 Nightingale
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Attribute
Bombardier CS300
×
McDonnell Douglas C-9 Nightingale
×
General
Manufacturer
Bombardier Aerospace
McDonnell Douglas
Model
Bombardier CS300
McDonnell Douglas C-9 Nightingale
Country
Canada
United States
Manufactured from (year)
2013
1968
Manufactured to (year)
-
1982
Type
Mid Size Passenger Jets
Military Aircraft
Icao
BCS3
DC9
Performance
Engine
2x Pratt And Whitney PW1500G
2x Pratt & Whitney JT8D-9
Power, lbf (lbf)
23,300
14,500
Avionics
Rockwell Collins Pro Line Fusion
-
Max cruise speed (km/h)
870
926
Approach speed (km/h)
259
235
Travel range (km)
6,112
3,221
Fuel economy (km/l)
0.396
-
Service ceiling (m)
12,497
11,278
Rate of climb (m/sec)
15.75
15.24
Take off distance (m)
1,890
2,100
Landing distance (m)
1,509
1,500
Weights
Max take off weight (kg)
67,585
50,000
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
84
Seats - business class
12
-
Cabin height (m)
2.1
2.05
Cabin width (m)
3.28
2.66
Cabin length (m)
27.5
-
Exterior length (m)
38.7
36.36
Tail height (m)
11.5
8.5
Fuselage diameter (m)
3.7
3.3
Wing span (m)
35.1
28.44
Wing tips
Blended Tips
No Winglets
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