Comparison of VC-25A Air Force One and McDonnell Douglas MD-11

Attribute	VC-25A Air Force One ×	McDonnell Douglas MD-11 ×
General
Manufacturer	Boeing	McDonnell Douglas
Model	VC-25A Air Force One	McDonnell Douglas MD-11
Country	United States	United States
Manufactured from (year)	1986	1988
Manufactured to (year)	1990	2000
Type	Heavy Business Jets	Jumbo Passenger Jets
Icao	VC25	MD11
Performance
Engine	4x General Electric CF6-80C2B1	3x 3 X Pratt & Whitney PW4460/62 or General Electric CF6-80C2D1F
Power, lbf (lbf)	56,700	61,500
Avionics	-	Honeywell VIA 2000 computers
Max cruise speed (km/h)	1,015	961
Approach speed (km/h)	278	278
Travel range (km)	12,686	13,408
Fuel economy (km/l)	0.064	0.093
Service ceiling (m)	13,746	13,106
Rate of climb (m/sec)	7.62	10.16
Take off distance (m)	3,190	3,139
Landing distance (m)	2,438	2,118
Weights
Max take off weight (kg)	377,842	285,988
Max landing weight (kg)	285,763	207,749
Max payload (kg)	68,180	66,549
Fuel tank capacity (l)	202,939	157,529
Baggage volume (m³)	28.3	150
Dimensions
Seats	12	41
Seats - business class	-	323
Seats - first class	-	293
Cabin height (m)	2.54	2.41
Cabin width (m)	6.13	5.71
Cabin length (m)	57	46.51
Exterior length (m)	70.6	61.62
Tail height (m)	19.33	17.65
Fuselage diameter (m)	6.49	6
Wing span (m)	59.6	51.97
Wing tips	Raked Wingtips	Canted Winglets