



| Name | VC-25A |
| Manufacturer | Boeing |
| Country of Origin | United States |
| Introduction / In Service Since | 1990 |
| Status | Active |
| Category | Presidential Strategic Airlift Aircraft |
| Crew | Approx. 26 |
| Unit Cost | Approx. $325 million |
| Length | 231 ft 10 in |
| Wingspan | 195 ft 8 in |
| Height | 63 ft 5 in |
| Wing Area | 5,500 sq ft |
| Empty Weight | Approx. 416,000 lb |
| Maximum Takeoff Weight (MTOW) | 833,000 lb |
| Maximum Speed | 630 mph |
| Range | 7,800+ miles |
| Combat Radius | Not applicable |
| Service Ceiling | 45,100 ft |
| Rate of Climb | Approx. 2,500 ft/min |
| Engine Type | 4 × GE CF6-80C2B1 turbofans |
| Thrust (per engine) | 56,700 lbf |
| Total Thrust | 226,800 lbf |
| Internal Payload Capacity | Classified |
| Weapons Bay | None |
| Compatible Weapons | None |
| Hardpoints | None |
| Radar System | Military-grade navigation radar |
| Navigation | Advanced GPS and inertial navigation |
| Electronic Warfare (EW) | Missile warning and countermeasure systems |
| Stealth Features | Limited infrared and electronic protection |
| Primary Operator | United States Air Force |
| Conflict Usage | Gulf War, post-9/11 operations |
| Notable Missions | Presidential global transport missions |
| Variants | VC-25A |
| Successor / Future Replacement | VC-25B |
The VC-25A is one of the most recognizable military aircraft in the world, serving as the primary presidential air transport platform for the United States. Commonly known by the radio callsign Air Force One when carrying the U.S. president, the aircraft is a heavily modified version of the Boeing 747-200B commercial airliner designed for secure global travel, command and control operations, and national continuity missions.
The aircraft combines long range performance, advanced communications systems, and survivability upgrades. Its role extends beyond VIP transport, functioning as an airborne command center capable of operating during national emergencies. The VC-25A fleet entered service in 1990 and remains a critical component of U.S. strategic mobility.
The VC-25A was developed and manufactured by Boeing in partnership with the U.S. Air Force. The aircraft was built in the United States and customized extensively with military-grade avionics, encrypted communications, aerial refueling capability, and defensive countermeasure systems.
Two VC-25A aircraft are operated by the Presidential Airlift Group under the 89th Airlift Wing stationed at Joint Base Andrews.
Powered by four General Electric CF6-80C2B1 turbofan engines, the VC-25A can reach a maximum speed of approximately 630 mph (Mach 0.92). The aircraft has an operational range exceeding 7,800 miles without refueling, allowing nonstop intercontinental travel.
One of its most important capabilities is aerial refueling, which theoretically allows the aircraft to remain airborne for extended durations during crisis operations.
The estimated procurement cost of each VC-25A aircraft exceeded $325 million at the time of acquisition in the late 1980s. Including modernization, communications infrastructure, and mission equipment, the overall program value is substantially higher today.
The aircraft is expected to be replaced in the coming years by the newer VC-25B platform based on the Boeing 747-8 airframe.
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