Comparison of Airbus A380-800 and VC-25A Air Force One

Attribute	Airbus A380-800 ×	VC-25A Air Force One ×
General
Manufacturer	Airbus	Boeing
Model	Airbus A380-800	VC-25A Air Force One
Country	France	United States
Manufactured from (year)	2007	1986
Manufactured to (year)	-	1990
Type	Jumbo Passenger Jets	Heavy Business Jets
Icao	A380	VC25
Performance
Engine	4x Engine Alliance GP7270 or Rolls-Royce Trent 900	4x General Electric CF6-80C2B1
Power, lbf (lbf)	81,500	56,700
Avionics	Thales Rockwell Honeywell Combo	-
Max cruise speed (km/h)	1,087	1,015
Approach speed (km/h)	250	278
Travel range (km)	14,816	12,686
Fuel economy (km/l)	0.049	0.064
Service ceiling (m)	13,106	13,746
Rate of climb (m/sec)	7.62	7.62
Take off distance (m)	2,749	3,190
Landing distance (m)	1,524	2,438
Weights
Max take off weight (kg)	575,000	377,842
Max landing weight (kg)	395,000	285,763
Max payload (kg)	87,000	68,180
Fuel tank capacity (l)	323,546	202,939
Baggage volume (m³)	190	28.3
Dimensions
Seats	853	12
Seats - business class	48	-
Seats - first class	416	-
Cabin height (m)	3	2.54
Cabin width (m)	6.58	6.13
Cabin length (m)	50.68	57
Exterior length (m)	72.73	70.6
Tail height (m)	24.27	19.33
Fuselage diameter (m)	7.14	6.49
Wing span (m)	79.75	59.6
Wing tips	Wingtip Fences	Raked Wingtips