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| Name | Boeing C-40C Clipper |
| Manufacturer | Boeing |
| Country of Origin | United States |
| Introduction / In Service Since | 2002 |
| Status | In operational service |
| Category | High-priority personnel transport |
| Crew | 10, mission dependent |
| Unit Cost | Approximately $70 million, historical figure |
| Length | 110 ft 4 in (33.6 m) |
| Wingspan | 117 ft 5 in (35.8 m) |
| Height | 41 ft 2 in (12.5 m) |
| Wing Area | Not publicly specified in the cited Air Force fact sheet |
| Empty Weight | Not publicly specified |
| Maximum Takeoff Weight (MTOW) | 171,000 lb (77,565 kg) |
| Maximum Speed | 530 mph (Mach 0.8) |
| Range | 4,500 to 5,000 nmi, payload dependent |
| Combat Radius | Not applicable |
| Service Ceiling | 41,000 ft (12,727 m) |
| Rate of Climb | 3,000 ft/min |
| Engine Type | 2 × GE CFM56-7B27 turbofans |
| Thrust (per engine) | 27,000 lb |
| Total Thrust | 54,000 lb |
| Internal Payload Capacity | 42 to 111 passengers |
| Weapons Bay | None |
| Compatible Weapons | None |
| Hardpoints | None |
| Radar System | Enhanced weather radar |
| Navigation | Integrated GPS and flight management system |
| Electronic Warfare (EW) | No dedicated combat EW suite publicly identified |
| Stealth Features | None |
| Primary Operator | U.S. Air Force, including Air National Guard and Air Force Reserve |
| Conflict Usage | Executive and operational support rather than direct combat |
| Notable Missions | Congressional delegations, Cabinet travel, senior leader transport, special envoys and diplomatic support |
| Variants | C-40B, C-40C |
| Successor / Future Replacement | No single direct replacement publicly designated |
| Notable Features | Reconfigurable cabin, winglets, military avionics and long-range capability |
| Estimated Operational Life | Dependent on airframe condition, modernization and sustainment |
The Boeing C-40C Clipper is a military executive transport aircraft operated by the U.S. Air Force for high-priority personnel movement, including congressional delegations, Cabinet officials, senior military leaders, special envoys, and other government passengers. Based on the Boeing 737-700 business jet, the C-40C combines a commercial airliner-derived airframe with military avionics, auxiliary fuel capacity, and a flexible passenger cabin. The aircraft entered U.S. military service in the early 2000s and was selected to replace older C-22 aircraft in its executive airlift role.
A major feature of the C-40C is its reconfigurable interior. Unlike the C-40B, which is optimized for combatant commanders and advanced airborne communications, the C-40C can be configured to carry approximately 42 to 111 passengers. This flexibility allows the aircraft to support distinguished visitor missions as well as larger personnel movements.
Boeing is the prime airframe contractor, while the aircraft uses two GE CFM56-7B27 turbofan engines. The C-40C incorporates the Boeing 737-700 fuselage with winglets and military-specific equipment, including integrated GPS, flight management systems, electronic flight instrumentation, a heads-up display, traffic collision avoidance technology, and enhanced weather radar.
The C-40C has a maximum speed of about 530 mph, or approximately Mach 0.8, and can operate at altitudes up to 41,000 feet. Its published unrefueled range is approximately 4,500 to 5,000 nautical miles, depending on payload. Each CFM56-7B27 engine produces about 27,000 pounds of static thrust.
The U.S. Air Force lists a historical unit cost of approximately $70 million for the C-40 family. This figure should be treated as a historical reference rather than a current procurement price, because configuration, support, modernization, inflation, and acquisition arrangements can significantly affect actual costs.
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