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/ Comparison of McDonnell Douglas DC-9-20 and McDonnell Douglas DC-9-30
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Comparison of McDonnell Douglas DC-9-20 and McDonnell Douglas DC-9-30
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Attribute
McDonnell Douglas DC-9-30
×
McDonnell Douglas DC-9-20
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General
Manufacturer
McDonnell Douglas
McDonnell Douglas
Model
McDonnell Douglas DC-9-30
McDonnell Douglas DC-9-20
Country
United States
United States
Manufactured from (year)
1965
1965
Manufactured to (year)
1982
1982
Type
Mid Size Passenger Jets
Mid Size Passenger Jets
Icao
DC93
DC92
Performance
Engine
2x JT8D-11
2x JT8D-11
Power, lbf (lbf)
15,000
15,000
Max cruise speed (km/h)
898
898
Approach speed (km/h)
235
235
Travel range (km)
2,778
2,778
Service ceiling (m)
10,668
10,668
Rate of climb (m/sec)
10.16
12.7
Take off distance (m)
2,100
1,600
Landing distance (m)
1,500
1,500
Weights
Max take off weight (kg)
48,988
45,359
Max landing weight (kg)
44,906
43,227
Max payload (kg)
13,674
11,501
Fuel tank capacity (l)
13,926
13,926
Baggage volume (m³)
25.3
17
Dimensions
Seats
115
9
Cabin height (m)
2.05
2.05
Cabin width (m)
3.12
3.12
Cabin length (m)
22.79
18.29
Exterior length (m)
36.36
31.82
Tail height (m)
8.5
8.4
Fuselage diameter (m)
3.35
3.35
Wing span (m)
28.44
28.44
Wing tips
No Winglets
No Winglets
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