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/ Comparison of VC-25A Air Force One and McDonnell Douglas DC-10-40
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Comparison of VC-25A Air Force One and McDonnell Douglas DC-10-40
[S]ave
Attribute
VC-25A Air Force One
×
McDonnell Douglas DC-10-40
×
General
Manufacturer
Boeing
McDonnell Douglas
Model
VC-25A Air Force One
McDonnell Douglas DC-10-40
Country
United States
United States
Manufactured from (year)
1986
1973
Manufactured to (year)
1990
1983
Type
Heavy Business Jets
Jumbo Passenger Jets
Icao
VC25
DC10
Performance
Engine
4x General Electric CF6-80C2B1
3x Pratt & Whitney JT9D-59A
Power, lbf (lbf)
56,700
53,000
Max cruise speed (km/h)
1,015
982
Approach speed (km/h)
278
276
Travel range (km)
12,686
9,445
Fuel economy (km/l)
0.064
-
Service ceiling (m)
13,746
12,802
Rate of climb (m/sec)
7.62
10.16
Take off distance (m)
3,190
3,000
Landing distance (m)
2,438
1,800
Weights
Max take off weight (kg)
377,842
251,744
Max landing weight (kg)
285,763
182,798
Max payload (kg)
68,180
44,356
Fuel tank capacity (l)
202,939
138,742
Baggage volume (m³)
28.3
130.7
Dimensions
Seats
12
399
Cabin height (m)
2.54
2.41
Cabin width (m)
6.13
5.7
Cabin length (m)
57
36.7
Exterior length (m)
70.6
55.5
Tail height (m)
19.33
17.7
Fuselage diameter (m)
6.49
6
Wing span (m)
59.6
50.4
Wing tips
Raked Wingtips
No Winglets
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