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Boeing C-32A
The C-32A has the body of the 757-200 but its own interior and 21st century avionics. Its cabin is in four sections: a forward communications center with 10 business class seats, a closed stateroom with a bed, a conference and staff area with eight seats, and a rear section with 32 seats, 45 passengers in all. Two Pratt and Whitney 2040 engines of 41,700 pounds of thrust each and a fuel load of 92,000 pounds give it an unrefueled range of 5,500 nautical miles. Its cruise speed is 537 miles per hour and it can use runways down to 5,000 feet. The crew is 16 and varies with the mission.
- Range
- 6,330 miles (5,500 nm, 10,190 km) unrefueled
- Cruise speed
- 467 knots (860 km/h)
- Engines
- Two Pratt and Whitney 2040 turbofans under the wings
- Max takeoff weight
- 255,000 lb (115,668 kg)
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Specifications
| Length | 155 ft 3 in (47.32 m) |
|---|---|
| Wingspan | 124 ft 8 in (38.00 m) |
| Height | 44 ft 6 in (13.56 m) |
| Ceiling | 42,000 ft (12,800 m) |
| Entry into service | June 1998 |
| Number built | 4 built |
| Status | In service |
| Type codes | Filed in flight plans as B752 (the code of an airliner type) |
Who flies it
- US Air Force (1st Airlift Squadron, 89th Airlift Wing)
Service branches, from the services' own fact sheets. No flight data is shown for military aircraft.