|A C-32A on final approach|
|Primary user||United States Air Force|
US$ 73.5 to 80 Million
|Developed from||Boeing 757|
The Boeing C-32, (Boeing 757-2G4), is a military passenger transport of the United States Air Force, providing transportation for United States leaders to locations around the world. The primary users are the Vice President of the United States (using the distinctive call sign "Air Force Two"), the First Lady, and the Secretary of State. On rare occasions, other members of the U.S. Cabinet and Congressional leaders have been authorized to fly aboard the C-32 for various missions. The C-32, since its debut, has also served as Air Force One in place of the larger VC-25A to airports that cannot accommodate the Boeing 747-based 'jumbo' jet.
Design and development
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A contract was awarded in August 1996 for four aircraft supplemented by the smaller C-37A to replace the aging fleet of VC-137 aircraft. The first aircraft was delivered to the 89th Airlift Wing at Andrews Air Force Base, Maryland in late June 1998.
Two further second-hand Boeing 757s were acquired in 2010 for government use although it is not clear which agency they are operated by; they have been frequently associated with the Foreign Emergency Support Team of the U.S. State Department.
The four C-32As are operated by the 1st Airlift Squadron of the 89th Airlift Wing. They are available for use by the vice-president (using call sign Air Force Two), the first lady and members of the cabinet and congress. They are also used by the President (using call sign Air Force One) if the destination is too small to take the larger VC-25.
- United States Air Force
- Crew: 2 + 1 jump seat + 13 mission crew
- Capacity: 45
- Length: 155 ft 3 in (47.32 m)
- Wingspan: 124 ft 10 in (38.05 m)
- Height: 44 ft 3 in (13.49 m) at MTOW
- Wing area: 185.25 sq ft (17.210 m2)
- Empty weight: 128,730 lb (58,391 kg) OWE
- Maximum zero-fuel weight: 186,000 lb (84,368 kg) MZFW
- Max takeoff weight: 256,000 lb (116,120 kg) MTOW
- Maximum landing weight: 210,000 lb (95,254 kg) MLW
- Fuel capacity: 13,334 US gal (11,103 imp gal; 50,475 l) with auxiliary tanks in fwd and aft catgo holds
- Potable water: 100 US gal (83 imp gal; 379 l)
- Runway LCN: 36 at ramp weight of 221,000 lb (100,244 kg), optimum tyre presures and subgrade C flexible pavement (LCN - Load classification number)
- Powerplant: 2 × Pratt & Whitney F117-PW-100 turbofan engines, 43,730 lbf (194.5 kN) thrust each
- (military Pratt & Whitney PW2040)
- Maximum speed: 526 kn (605 mph, 974 km/h)
- Maximum speed: Mach 0.86 (MMO)
- Cruising speed: Mach 0.8
- Approach speed: 137 kn (158 mph; 254 km/h)
- Initial cruising height: 35,400 ft (10,790 m)
- Range: 5,650 nmi (6,500 mi, 10,460 km)
- Service ceiling: 42,000 ft (13,000 m)
- Wing loading: 127.88 lb/sq ft (624.4 kg/m2)
- Thrust/weight: 0.314
- Take-off field length: 7,800 ft (2,377 m) at sea level 29 °C (84 °F)
- Landing field length: 5,100 ft (1,554 m) at MLW
mission avionics + satcom
Aircraft of comparable role, configuration and era
- Air Force C-32 factsheet. US Air Force, 12 May 2015.
- "Programs and Initiatives". state.gov. Retrieved 4 April 2018.
- "Foreign Emergency Support Team (FEST)". US Department of State. Retrieved on May 8, 2013
- Weisgerber, Marcus. "Pentagon Wants to Get Started on New Air Force Two and Doomsday Planes". Defense One. Retrieved 24 August 2017.
- Jackson, Paul, ed. (2003). Jane's All the World's Aircraft 2003-04 (94th ed.). Coulsdon, Surrey, United Kingdom: Jane's Information Group. pp. 569–571. ISBN 0-7106-2537-5.
- The original version of this article was from the public domain source at Air Force Link
|Wikimedia Commons has media related to Boeing C-32.|
- U.S. Air Force C-32 factsheet. US Air Force, 12 May 2015.]