Specifications |
Primary Function | Presidential air transport |
Contractor | Boeing Airplane Co. |
Power Plant | Four General Electric CF6-80C2B1 jet engines |
Thrust | 56,700 pounds, each engine |
Length | 231 feet, 10 inches (70.7 meters) |
Height | 63 feet, 5 inches (19.3 meters) |
Wingspan | 195 feet, 8 inches (59.6 meters) |
Speed | 630 miles per hour (Mach 0.92) |
Ceiling | 45,100 feet (13,746 meters) |
Maximum Takeoff Weight | 833,000 pounds (374,850 kilograms) |
Range | 7,800 statute miles (6,800 nautical miles) (12,550 kilometers) |
Crew | 26 (passenger/crew capacity: 102) |
Introduction Date | Dec. 8, 1990 (tail No. 28000); Dec. 23, 1990 (tail No. 29000) |
Date Deployed | Sept. 6, 1990 (tail No. 28000); Mar. 26, 1991 (tail No. 29000) |
Inventory | Active force, 2; ANG, 0; Reserve, 0 |