| 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
|
| Systems |
AN/ALQ-204 HAVE CHARCOAL IRCM ..... or
AN/AAQ-24 Directional Infrared Countermeasures (DIRCM)
COMBAT CIDERS full-duplex frequency division multiplexing (FDM) multi-channel Air Force One communications link, via nuclear-hardened antennas at many of the AUTOVON switching centers. Synonymous with AUTOVON WIDEBAND.
|
